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: 11 hours ago
TLE from 11 hours ago
0 GGSE 2
1 1244U 65016B 26196.22206285 -.00000009 00000-0 31375-4 0 9993
2 1244 70.0791 126.6011 0018997 46.8765 313.3926 13.96164512121979Epoch: 2026-07-15T05:19Z
TLE epoch observation values (Epoch: 2026-07-15T05:19:46.230Z)
Latitude
-0.00004°
Longitude
113.57749°
Altitude
899.93 km
Speed
7.407 km/s
True Right ascension
08h 26m 24s
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
05:19:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
918.978 km
Perigee altitude
891.306 km
Semi-major axis
7,283.279 km
Eccentricity
0.0019
Inclination
70.0791°
RAAN
126.6011°
Arg. of periapsis
46.8765°
True anomaly
313.23415°
Mean anomaly
313.3926°
Eccentric anomaly
313.3134°
Mean motion
3.49183 °/min
Orbital period
103.1 mins
BSTAR
0.000031375
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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 | 2026-07-15 19:14:07.007Z | 115.883° SE | 2026-07-15 19:16:07.007Z | 94.913° ESE | 12.323° | 2026-07-15 19:18:07.007Z | 74.573° E |
| 10 mins | 2026-07-15 20:56:07.007Z | 205.762° SW | 2026-07-15 21:00:07.007Z | 224.944° SW | 44.078° | 2026-07-15 21:06:07.007Z | 23.183° NE |
| 5 mins | 2026-07-15 22:45:07.007Z | 291.843° WNW | 2026-07-15 22:47:07.007Z | 313.994° NW | 14.354° | 2026-07-15 22:50:07.007Z | 345.613° N |
| 10 mins | 2026-07-16 05:58:07.007Z | 348.434° N | 2026-07-16 06:02:07.007Z | 45.626° ENE | 38.952° | 2026-07-16 06:08:07.007Z | 138.778° SSE |
| 6 mins | 2026-07-16 07:45:07.007Z | 290.907° WNW | 2026-07-16 07:48:07.007Z | 252.105° W | 20.123° | 2026-07-16 07:51:07.007Z | 217.824° 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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