diff --git a/SPG4Tool/PassPredict.cpp b/SPG4Tool/PassPredict.cpp
new file mode 100644
index 0000000..a1148a9
--- /dev/null
+++ b/SPG4Tool/PassPredict.cpp
@@ -0,0 +1,402 @@
+#include <Observer.h>
+#include <SGP4.h>
+#include <Util.h>
+#include <CoordTopocentric.h>
+#include <CoordGeodetic.h>
+
+#include <cmath>
+#include <iostream>
+#include <list>
+#include <QDate>
+#include <QDateTime>
+#include <iomanip>
+#include <sstream>
+
+#include "SPG4Function.h"
+
+struct PassDetails
+{
+    libsgp4::DateTime aos;
+    libsgp4::DateTime los;
+    double max_elevation;
+};
+
+double FindMaxElevation(
+    const libsgp4::CoordGeodetic& user_geo,
+    libsgp4::SGP4& sgp4,
+    const libsgp4::DateTime& aos,
+    const libsgp4::DateTime& los)
+{
+    libsgp4::Observer obs(user_geo);
+
+    bool running;
+
+    double time_step = (los - aos).TotalSeconds() / 9.0;
+    libsgp4::DateTime current_time(aos); //! current time
+    libsgp4::DateTime time1(aos); //! start time of search period
+    libsgp4::DateTime time2(los); //! end time of search period
+    double max_elevation; //! max elevation
+
+    running = true;
+
+    do
+    {
+        running = true;
+        max_elevation = -99999999999999.0;
+        while (running && current_time < time2)
+        {
+            /*
+             * find position
+             */
+            libsgp4::Eci eci = sgp4.FindPosition(current_time);
+            libsgp4::CoordTopocentric topo = obs.GetLookAngle(eci);
+
+            if (topo.elevation > max_elevation)
+            {
+                /*
+                 * still going up
+                 */
+                max_elevation = topo.elevation;
+                /*
+                 * move time along
+                 */
+                current_time = current_time.AddSeconds(time_step);
+                if (current_time > time2)
+                {
+                    /*
+                     * dont go past end time
+                     */
+                    current_time = time2;
+                }
+            }
+            else
+            {
+                /*
+                 * stop
+                 */
+                running = false;
+            }
+        }
+
+        /*
+         * make start time to 2 time steps back
+         */
+        time1 = current_time.AddSeconds(-2.0 * time_step);
+        /*
+         * make end time to current time
+         */
+        time2 = current_time;
+        /*
+         * current time to start time
+         */
+        current_time = time1;
+        /*
+         * recalculate time step
+         */
+        time_step = (time2 - time1).TotalSeconds() / 9.0;
+    } while (time_step > 1.0);
+
+    return max_elevation;
+}
+
+libsgp4::DateTime FindCrossingPoint(
+    const libsgp4::CoordGeodetic& user_geo,
+    libsgp4::SGP4& sgp4,
+    const libsgp4::DateTime& initial_time1,
+    const libsgp4::DateTime& initial_time2,
+    bool finding_aos)
+{
+    libsgp4::Observer obs(user_geo);
+
+    bool running;
+    int cnt;
+
+    libsgp4::DateTime time1(initial_time1);
+    libsgp4::DateTime time2(initial_time2);
+    libsgp4::DateTime middle_time;
+
+    running = true;
+    cnt = 0;
+    while (running && cnt++ < 16)
+    {
+        middle_time = time1.AddSeconds((time2 - time1).TotalSeconds() / 2.0);
+        /*
+         * calculate satellite position
+         */
+        libsgp4::Eci eci = sgp4.FindPosition(middle_time);
+        libsgp4::CoordTopocentric topo = obs.GetLookAngle(eci);
+
+        if (topo.elevation > 0.0)
+        {
+            /*
+             * satellite above horizon
+             */
+            if (finding_aos)
+            {
+                time2 = middle_time;
+            }
+            else
+            {
+                time1 = middle_time;
+            }
+        }
+        else
+        {
+            if (finding_aos)
+            {
+                time1 = middle_time;
+            }
+            else
+            {
+                time2 = middle_time;
+            }
+        }
+
+        if ((time2 - time1).TotalSeconds() < 1.0)
+        {
+            /*
+             * two times are within a second, stop
+             */
+            running = false;
+            /*
+             * remove microseconds
+             */
+            int us = middle_time.Microsecond();
+            middle_time = middle_time.AddMicroseconds(-us);
+            /*
+             * step back into the pass by 1 second
+             */
+            middle_time = middle_time.AddSeconds(finding_aos ? 1 : -1);
+        }
+    }
+
+    /*
+     * go back/forward 1second until below the horizon
+     */
+    running = true;
+    cnt = 0;
+    while (running && cnt++ < 6)
+    {
+        libsgp4::Eci eci = sgp4.FindPosition(middle_time);
+        libsgp4::CoordTopocentric topo = obs.GetLookAngle(eci);
+        if (topo.elevation > 0)
+        {
+            middle_time = middle_time.AddSeconds(finding_aos ? -1 : 1);
+        }
+        else
+        {
+            running = false;
+        }
+    }
+
+    return middle_time;
+}
+
+std::list<struct PassDetails> GeneratePassList(
+    const libsgp4::CoordGeodetic& user_geo,
+    libsgp4::SGP4& sgp4,
+    const libsgp4::DateTime& start_time,
+    const libsgp4::DateTime& end_time,
+    const int time_step)
+{
+    std::list<struct PassDetails> pass_list;
+
+    libsgp4::Observer obs(user_geo);
+
+    libsgp4::DateTime aos_time;
+    libsgp4::DateTime los_time;
+
+    bool found_aos = false;
+
+    libsgp4::DateTime previous_time(start_time);
+    libsgp4::DateTime current_time(start_time);
+
+    while (current_time < end_time)
+    {
+        bool end_of_pass = false;
+
+        /*
+         * calculate satellite position
+         */
+        libsgp4::Eci eci = sgp4.FindPosition(current_time);
+        libsgp4::CoordTopocentric topo = obs.GetLookAngle(eci);
+
+        if (!found_aos && topo.elevation > 0.0)
+        {
+            /*
+             * aos hasnt occured yet, but the satellite is now above horizon
+             * this must have occured within the last time_step
+             */
+            if (start_time == current_time)
+            {
+                /*
+                 * satellite was already above the horizon at the start,
+                 * so use the start time
+                 */
+                aos_time = start_time;
+            }
+            else
+            {
+                /*
+                 * find the point at which the satellite crossed the horizon
+                 */
+                aos_time = FindCrossingPoint(
+                    user_geo,
+                    sgp4,
+                    previous_time,
+                    current_time,
+                    true);
+            }
+            found_aos = true;
+        }
+        else if (found_aos && topo.elevation < 0.0)
+        {
+            found_aos = false;
+            /*
+             * end of pass, so move along more than time_step
+             */
+            end_of_pass = true;
+            /*
+             * already have the aos, but now the satellite is below the horizon,
+             * so find the los
+             */
+            los_time = FindCrossingPoint(
+                user_geo,
+                sgp4,
+                previous_time,
+                current_time,
+                false);
+
+            struct PassDetails pd;
+            pd.aos = aos_time;
+            pd.los = los_time;
+            pd.max_elevation = FindMaxElevation(
+                user_geo,
+                sgp4,
+                aos_time,
+                los_time);
+
+            pass_list.push_back(pd);
+        }
+
+        /*
+         * save current time
+         */
+        previous_time = current_time;
+
+        if (end_of_pass)
+        {
+            /*
+             * at the end of the pass move the time along by 30mins
+             */
+            current_time = current_time + libsgp4::TimeSpan(0, 30, 0);
+        }
+        else
+        {
+            /*
+             * move the time along by the time step value
+             */
+            current_time = current_time + libsgp4::TimeSpan(0, 0, time_step);
+        }
+
+        if (current_time > end_time)
+        {
+            /*
+             * dont go past end time
+             */
+            current_time = end_time;
+        }
+    };
+
+    if (found_aos)
+    {
+        /*
+         * satellite still above horizon at end of search period, so use end
+         * time as los
+         */
+        struct PassDetails pd;
+        pd.aos = aos_time;
+        pd.los = end_time;
+        pd.max_elevation = FindMaxElevation(user_geo, sgp4, aos_time, end_time);
+        pass_list.push_back(pd);
+    }
+
+    return pass_list;
+}
+
+
+bool PassPredict(std::vector<QDateTime>& aos, std::vector<QDateTime>& los, std::string line1, std::string line2, double startTime, double predictDayLen, double lon, double lat, double ati) {
+
+    libsgp4::CoordGeodetic geo(lat, lon, ati);
+    libsgp4::Tle tle("GALILEO-PFM (GSAT0101)  ",
+        line1,
+        line2);
+    libsgp4::SGP4 sgp4(tle);
+
+	std::vector<QDateTime> result;
+
+    // 将 double 时间戳转为 QDateTime
+ 
+    QDateTime dateTime = QDateTime::fromSecsSinceEpoch(static_cast<qint64>(startTime*1000));
+
+
+    libsgp4::DateTime start_date(
+		dateTime.date().year(),
+		dateTime.date().month(),
+		dateTime.date().day(),
+		dateTime.time().hour(),
+		dateTime.time().minute(),
+		dateTime.time().second(),
+		dateTime.time().msec() * 1000);
+
+    libsgp4::DateTime end_date(start_date.AddDays(predictDayLen));
+
+    std::list<struct PassDetails> pass_list;
+    pass_list = GeneratePassList(geo, sgp4, start_date, end_date, 180);
+
+    if (pass_list.begin() == pass_list.end())
+    {
+        return false;
+    }
+    else
+    {
+        std::stringstream ss;
+        ss << std::right << std::setprecision(1) << std::fixed;
+        std::list<struct PassDetails>::const_iterator itr = pass_list.begin();
+        do
+        {
+            ss << "AOS: " << itr->aos
+                << ", LOS: " << itr->los
+                << ", Max El: " << std::setw(4) << libsgp4::Util::RadiansToDegrees(itr->max_elevation)
+                << ", Duration: " << (itr->los - itr->aos)
+                << std::endl;
+
+
+            // 构造AOS时间
+            QDate aosDate(itr->aos.Year(), itr->aos.Month(), itr->aos.Day());
+            QTime aosTimePart(itr->aos.Hour(), itr->aos.Minute(), itr->aos.Second(), itr->aos.Microsecond());
+            QDateTime aosDateTime(aosDate, aosTimePart, Qt::UTC); // 
+
+            // 构造LOS时间
+            QDate losDate(itr->los.Year(), itr->los.Month(), itr->los.Day());
+            QTime losTimePart(itr->los.Hour(), itr->los.Minute(), itr->los.Second(), itr->los.Microsecond());
+            QDateTime losDateTime(losDate, losTimePart, Qt::UTC); // 
+
+			aos.push_back(aosDateTime);
+			los.push_back(losDateTime);
+
+
+
+        } while (++itr != pass_list.end());
+        std::cout << ss.str();
+
+        return true;
+
+    }
+
+    return false;
+
+}
+
+
+ 
\ No newline at end of file
diff --git a/SPG4Tool/SPG4Function.h b/SPG4Tool/SPG4Function.h
index c9c8b81..4e99725 100644
--- a/SPG4Tool/SPG4Function.h
+++ b/SPG4Tool/SPG4Function.h
@@ -4,10 +4,11 @@
 #include "SPG4Tool_global.h"
 #include "BaseConstVariable.h"
 #include <vector>
-
+#include <QDateTime>
 //void RunTle(libsgp4::Tle tle, double start, double end, double inc);
 
 
+
 SPG4TOOL_EXPORT double parseTLETimeOffset(const std::string& tle);
 /// <summary>
 /// 根据两行根数生成坐标与速度，请注意返回的单位是 km
@@ -22,4 +23,7 @@ SPG4TOOL_EXPORT double parseTLETimeOffset(const std::string& tle);
 /// <param name="first_run"></param>
 /// <returns></returns>
 SPG4TOOL_EXPORT std::vector<SatelliteAntPos> getGPSPoints(std::string line1, std::string line2, double start, double end, double inc, bool printfinfoflag = false, bool running = true, bool first_run = true);
+SPG4TOOL_EXPORT bool PassPredict(std::vector<QDateTime>& aos, std::vector<QDateTime>& los, std::string line1, std::string line2, double startTime, double predictDayLen, double lon, double lat, double ati);
+
+
 #endif
diff --git a/SPG4Tool/SPG4Tool.h b/SPG4Tool/SPG4Tool.h
index 40103f3..cf443e1 100644
--- a/SPG4Tool/SPG4Tool.h
+++ b/SPG4Tool/SPG4Tool.h
@@ -8,6 +8,11 @@
 #include <list>
 #include <string>
 #include "BaseConstVariable.h"
- 
+#include <Observer.h>
+#include <SGP4.h>
+#include <Util.h>
+#include <CoordTopocentric.h>
+#include <CoordGeodetic.h>
+
 
 std::vector<SatelliteAntPos> RunTle(libsgp4::Tle tle, double start, double end, double inc, bool printfinfoflag, bool running = true, bool first_run = true);
diff --git a/SPG4Tool/SPG4Tool.vcxproj b/SPG4Tool/SPG4Tool.vcxproj
index 878cdae..1b5bd90 100644
--- a/SPG4Tool/SPG4Tool.vcxproj
+++ b/SPG4Tool/SPG4Tool.vcxproj
@@ -115,6 +115,7 @@
     <ClCompile Include="libsgp4\TleException.cc" />
     <ClCompile Include="libsgp4\Util.cc" />
     <ClCompile Include="libsgp4\Vector.cc" />
+    <ClCompile Include="PassPredict.cpp" />
     <ClCompile Include="SPG4Toolmain.cpp" />
     <ClCompile Include="SPG4Function.cpp" />
   </ItemGroup>
diff --git a/SPG4Tool/SPG4Tool.vcxproj.filters b/SPG4Tool/SPG4Tool.vcxproj.filters
index e658568..d2d7c1f 100644
--- a/SPG4Tool/SPG4Tool.vcxproj.filters
+++ b/SPG4Tool/SPG4Tool.vcxproj.filters
@@ -80,6 +80,9 @@
     <ClCompile Include="SPG4Function.cpp">
       <Filter>Source Files</Filter>
     </ClCompile>
+    <ClCompile Include="PassPredict.cpp">
+      <Filter>Source Files</Filter>
+    </ClCompile>
   </ItemGroup>
   <ItemGroup>
     <ClInclude Include="libsgp4\CoordGeodetic.h">