08 Dec 2006 19:34:30 Satellite-Ahead_FDF282 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 08:30:31.142 [2454081.85452711]: Stopped on: Periapsis; Run Sequence STOP Propagation Statistics: Number of steps: 83 Average step size: 5406.33 sec Largest step size: 30808.5 sec Smallest step size: 18.4222 sec ---------------------------------- Satellite State at End of Segment: ---------------------------------- UTC Gregorian Date: 12 Dec 2006 08:30:31.142 UTC Julian Date: 2454081.85452711 Julian Ephemeris Date: 2454081.85528155 Time past epoch: 2.98386e+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: 10664.4949154364710000 km Vx: -3.4577954388210963 km/sec Y: 7068.0099183344055000 km Vy: 6.2560599235085999 km/sec Z: 2553.4639470207580000 km Vz: -2.8754084187797604 km/sec Parameter Set Type: Keplerian sma: 228756.4120456079300000 km RAAN: 238.9705968332609 deg ecc: 0.9429681826339402 w: 152.3256650884856 deg inc: 24.92362303465632 deg TA: 359.9999999798132 deg Parameter Set Type: Spherical Right Asc: 33.53485954126611 deg Horiz. FPA: -9.797135756705807e-009 deg Decl: 11.28689332199413 deg Azimuth: 112.3684665303303 deg |R|: 13046.3939131002280000 km |V|: 7.7047134040178245 km/sec Other Elliptic Orbit Parameters : Ecc. Anom: 360 deg Mean Anom: 360 deg Long Peri: 31.29626192174646 deg Arg. Lat: 152.3256650682988 deg True Long: 31.29626190155966 deg Vert FPA: 90.00000000979712 deg Ang. Mom: 100518.7260563599 km^2/sec p: 25348.7282712628510000 km C3: -1.742466749830513 km^2/sec^2 Energy: -0.8712333749152563 km^2/sec^2 Vel. RA: 118.9299277638873 deg Vel. Decl: -21.9131806183325 deg Rad. Peri: 13046.3939131002280000 km Vel. Peri: 7.7047134040178245 km/sec Rad. Apo: 444466.4301781156100000 km Vel. Apo: 0.2261559461669084 km/sec Mean Mot.: 0.0003306218913607335 deg/sec Period: 1088857.11868127 sec Period: 18147.61864468783 min Period: 302.4603107447971 hr Period: 12.60251294769988 day Time Past Periapsis: 1088857.11868127 sec Time Past Ascending Node: 57434.46190525068 sec Beta Angle (Orbit plane to Sun): -29.2980025764852 deg Mean Sidereal Greenwich Hour Angle: 208.534362723768 deg Geodetic Parameters: Latitude: 11.35684781633829 deg Longitude: -174.9066050814049 deg Altitude: 6669.0822076431250000 km Geocentric Parameters: Latitude: 11.32064082630426 deg Longitude: -174.9066050814049 deg Spacecraft Configuration: Drag Area: 7.436e-006 km^2 SRP Area: 7.436e-006 km^2 Dry Mass: 561.36 kg Fuel Mass: 43.58 kg Total Mass: 604.94 kg Area/Mass Ratio: 1.22921e-008 km^2/kg Tank Pressure: 1390734.598847697 Pa Fuel Density: 1007300000000 kg/km^3 Cr: 1.391729 Cd: 2.000000 User-selected results: Altitude = 6669.0822076431250000 km Altitude Of Periapsis = 6668.2569131002274000 km R Mag = 13046.3939131002280000 km