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: 13 hours ago
TLE from 13 hours ago
0 GGSE 2
1 01244U 65016B 26308.27189495 .00000008 00000-0 44227-4 0 9994
2 01244 70.0790 247.8987 0023821 265.4164 94.4222 13.96179062137610Epoch: 2026-11-04T06:31Z
TLE epoch observation values (Epoch: 2026-11-04T06:31:31.723Z)
Latitude
0.00003°
Longitude
106.49394°
Altitude
910.754 km
Speed
7.396 km/s
True Right ascension
16h 31m 35s
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
15:13:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
922.441 km
Perigee altitude
887.742 km
Semi-major axis
7,283.228 km
Eccentricity
0.00238
Inclination
70.079°
RAAN
247.8987°
Arg. of periapsis
265.4164°
True anomaly
94.69429°
Mean anomaly
94.4222°
Eccentric anomaly
94.55825°
Mean motion
3.49186 °/min
Orbital period
103.1 mins
BSTAR
0.000044227
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-11-04 20:24:11.014Z | 146.576° SSE | 2026-11-04 20:28:11.014Z | 98.139° ESE | 23.804° | 2026-11-04 20:32:11.014Z | 53.698° ENE |
| 9 mins | 2026-11-04 22:09:11.014Z | 230.575° WSW | 2026-11-04 22:13:11.014Z | 300.97° NW | 51.564° | 2026-11-04 22:18:11.014Z | 12.406° NNE |
| 6 mins | 2026-11-05 05:26:11.014Z | 18.351° NNE | 2026-11-05 05:29:11.014Z | 51.569° ENE | 16.401° | 2026-11-05 05:32:11.014Z | 82.555° E |
| 11 mins | 2026-11-05 07:10:11.014Z | 335.574° NNW | 2026-11-05 07:15:11.014Z | 321.173° NNW | 88.359° | 2026-11-05 07:21:11.014Z | 157.636° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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