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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 GGSE 2
1 01244U 65016B 26044.55127929 .00000063 00000-0 83589-4 0 9991
2 01244 70.0779 89.6915 0023760 253.3306 106.5192 13.96138069100800Epoch: 2026-02-13T13:13Z
TLE epoch observation values (Epoch: 2026-02-13T13:13:50.530Z)
Latitude
-0.00002°
Longitude
107.64389°
Altitude
914.477 km
Speed
7.392 km/s
True Right ascension
05h 58m 45s
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
10:32:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
922.539 km
Perigee altitude
887.929 km
Semi-major axis
7,283.371 km
Eccentricity
0.00238
Inclination
70.0779°
RAAN
89.6915°
Arg. of periapsis
253.3306°
True anomaly
106.78001°
Mean anomaly
106.5192°
Eccentric anomaly
106.64963°
Mean motion
3.49176 °/min
Orbital period
103.1 mins
BSTAR
0.000083589
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-14 12:08:09.177Z | 16.452° NNE | 2026-02-14 12:11:09.177Z | 48.345° ENE | 14.721° | 2026-02-14 12:14:09.177Z | 79.159° E |
| 10 mins | 2026-02-14 13:53:09.177Z | 337.816° N | 2026-02-14 13:57:09.177Z | 8.493° NNE | 44.526° | 2026-02-14 14:03:09.177Z | 154.667° SSE |
| 8 mins | 2026-02-15 03:11:09.177Z | 153.143° SSE | 2026-02-15 03:15:09.177Z | 97.832° ESE | 26.43° | 2026-02-15 03:19:09.177Z | 49.924° ENE |
| 9 mins | 2026-02-15 04:56:09.177Z | 238.88° WSW | 2026-02-15 05:00:09.177Z | 299.551° NW | 33.697° | 2026-02-15 05:05:09.177Z | 8.37° NNE |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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