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, 1.9 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GGSE 2
1 01244U 65016B 26208.11487645 .00000032 00000-0 61055-4 0 9999
2 01244 70.0791 101.2679 0019589 30.0132 330.2093 13.96166082123631Epoch: 2026-07-27T02:45Z
TLE epoch observation values (Epoch: 2026-07-27T02:45:25.325Z)
Latitude
0.00002°
Longitude
115.1093°
Altitude
897.04 km
Speed
7.41 km/s
True Right ascension
06h 45m 04s
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
22:39:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
919.404 km
Perigee altitude
890.869 km
Semi-major axis
7,283.274 km
Eccentricity
0.00196
Inclination
70.0791°
RAAN
101.2679°
Arg. of periapsis
30.0132°
True anomaly
330.09754°
Mean anomaly
330.2093°
Eccentric anomaly
330.15344°
Mean motion
3.49183 °/min
Orbital period
103.1 mins
BSTAR
0.000061055
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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 | 2026-07-28 16:43:17.820Z | 128.422° SE | 2026-07-28 16:46:17.820Z | 94.866° ESE | 15.421° | 2026-07-28 16:49:17.820Z | 63.727° ENE |
| 10 mins | 2026-07-28 18:26:17.820Z | 214.159° SW | 2026-07-28 18:31:17.820Z | 327.872° NNW | 42.641° | 2026-07-28 18:36:17.820Z | 19.511° NNE |
| 10 mins | 2026-07-29 03:28:17.820Z | 343.675° N | 2026-07-29 03:33:17.820Z | 92.816° ESE | 41.939° | 2026-07-29 03:38:17.820Z | 145.558° SSE |
| 6 mins | 2026-07-29 05:15:17.820Z | 288.534° WNW | 2026-07-29 05:17:17.820Z | 266.083° W | 16.683° | 2026-07-29 05:21:17.820Z | 222.637° SW |
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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