08 Dec 2006 20:46:06 Satellite-Behind_FDF291 Astrogator MCS P4 Summary ----------------------------------------------------------------------------------------------- MCS Segment Type: Propagate Name: Phasing Orbit Sequence.P4 User Comment: -Perigee 4- Propagator model used: STEREO_Phasing (STEREO Phasing Orbit Propagator) Stopping Condition Information (Gregorian Date [Julian Date]): 12 Dec 2006 09:54:54.150 [2454081.91312674]: Stopped on: Periapsis; Run Sequence STOP Propagation Statistics: Number of steps: 81 Average step size: 4864.35 sec Largest step size: 27583.9 sec Smallest step size: 45.9315 sec ---------------------------------- Satellite State at End of Segment: ---------------------------------- UTC Gregorian Date: 12 Dec 2006 09:54:54.150 UTC Julian Date: 2454081.91312674 Julian Ephemeris Date: 2454081.91388119 Time past epoch: 2.98437e+007 sec (Epoch in UTC Gregorian Date: 1 Jan 2006 00:00:00.000) State Vector in Coordinate System: Earth Centered Mean J2000 Parameter Set Type: Cartesian X: 10677.1466507192450000 km Vx: -3.6605425636800293 km/sec Y: 7068.7192715317906000 km Vy: 6.3581836939265024 km/sec Z: 2486.2984340296944000 km Vz: -2.3569438976524957 km/sec Parameter Set Type: Keplerian sma: 229831.5374101628300000 km RAAN: 243.675759035438 deg ecc: 0.9432447202649541 w: 148.069706074368 deg inc: 21.12423218056995 deg TA: 359.9999998987232 deg Parameter Set Type: Spherical Right Asc: 33.50623137177609 deg Horiz. FPA: -4.915947366526368e-008 deg Decl: 10.98817221673831 deg Azimuth: 108.154084579581 deg |R|: 13044.1531976494610000 km |V|: 7.7059234542595449 km/sec Other Elliptic Orbit Parameters : Ecc. Anom: 360 deg Mean Anom: 360 deg Long Peri: 31.745465109806 deg Arg. Lat: 148.0697059730912 deg True Long: 31.74546500852915 deg Vert FPA: 90.00000004915947 deg Ang. Mom: 100517.2460667216 km^2/sec p: 25347.9818316595270000 km C3: -1.734315691795805 km^2/sec^2 Energy: -0.8671578458979024 km^2/sec^2 Vel. RA: 119.929956121126 deg Vel. Decl: -17.80999030656137 deg Rad. Peri: 13044.1531976494610000 km Vel. Peri: 7.7059234542595441 km/sec Rad. Apo: 446618.9216226762500000 km Vel. Apo: 0.2250626679709802 km/sec Mean Mot.: 0.0003283046900708163 deg/sec Period: 1096542.36106815 sec Period: 18275.70601780249 min Period: 304.5951002967082 hr Period: 12.69146251236284 day Time Past Periapsis: 1096542.36106815 sec Time Past Ascending Node: 43004.27335400786 sec Beta Angle (Orbit plane to Sun): -27.0404235326764 deg Mean Sidereal Greenwich Hour Angle: 229.687989069126 deg Geodetic Parameters: Latitude: 11.05723633858507 deg Longitude: 163.9110333768676 deg Altitude: 6666.7990483217991000 km Geocentric Parameters: Latitude: 11.02193011087062 deg Longitude: 163.9110333768676 deg Spacecraft Configuration: Drag Area: 7.436e-006 km^2 SRP Area: 7.436e-006 km^2 Dry Mass: 596.01 kg Fuel Mass: 47.27 kg Total Mass: 643.28 kg Area/Mass Ratio: 1.15595e-008 km^2/kg Tank Pressure: 1476601.906176816 Pa Fuel Density: 1007300000000 kg/km^3 Cr: 1.388146 Cd: 2.000000 User-selected results: Altitude = 6666.7990483217991000 km Altitude Of Periapsis = 6666.0161976494601000 km R Mag = 13044.1531976494610000 km