GGSE 2, 1244
Orbit data source: Space-Track
GGSE 2, 1244 is an American payload satellite in LEO that was launched on Tue, 09 Mar 1965 UTC via a THOR SLV-2 AGENA D launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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1244 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
NRL 24", Unknown motor
Mass
55 kg wet, 55 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
SPHERE + ANT, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 GGSE 2
1 01244U 65016B 26314.79138896 .00000047 00000-0 71920-4 0 9990
2 01244 70.0793 234.0107 0023728 257.8324 102.0124 13.96180105138522Epoch: 2026-11-10T18:59Z
TLE epoch observation values (Epoch: 2026-11-10T18:59:36.006Z)
Latitude
-0.00003°
Longitude
-100.83785°
Altitude
913.008 km
Speed
7.394 km/s
True Right ascension
15h 36m 02s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
03:25:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
922.369 km
Perigee altitude
887.806 km
Semi-major axis
7,283.225 km
Eccentricity
0.00237
Inclination
70.0793°
RAAN
234.0107°
Arg. of periapsis
257.8324°
True anomaly
102.27818°
Mean anomaly
102.0124°
Eccentric anomaly
102.14531°
Mean motion
3.49187 °/min
Orbital period
103.1 mins
BSTAR
0.00007192
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Other satellites on launch #16 in the year 1965 (1965-03-09 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GGSE 2 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-11-11 07:40:32.680Z | 284.008° WNW | 2026-11-11 07:42:32.680Z | 263.762° W | 12.866° | 2026-11-11 07:44:32.680Z | 243.234° WSW |
| 8 mins | 2026-11-11 19:11:32.680Z | 153.813° SSE | 2026-11-11 19:15:32.680Z | 97.238° ESE | 30.708° | 2026-11-11 19:19:32.680Z | 49.219° ENE |
| 9 mins | 2026-11-11 20:56:32.680Z | 240.062° WSW | 2026-11-11 21:00:32.680Z | 300.207° NW | 40.825° | 2026-11-11 21:05:32.680Z | 7.926° NNE |
| 7 mins | 2026-11-12 04:13:32.680Z | 15.638° NNE | 2026-11-12 04:16:32.680Z | 51.619° ENE | 20.291° | 2026-11-12 04:20:32.680Z | 94.813° ESE |
| 10 mins | 2026-11-12 05:58:32.680Z | 328.216° NNW | 2026-11-12 06:02:32.680Z | 253.347° W | 70.825° | 2026-11-12 06:08:32.680Z | 166.426° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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