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: 17 hours ago
TLE from 17 hours ago
0 GGSE 2
1 01244U 65016B 26134.60842343 -.00000001 00000-0 37247-4 0 9994
2 01244 70.0792 257.8478 0019196 138.3202 221.9371 13.96155482113378Epoch: 2026-05-14T14:36Z
TLE epoch observation values (Epoch: 2026-05-14T14:36:07.784Z)
Latitude
-0.00003°
Longitude
166.46371°
Altitude
919.873 km
Speed
7.387 km/s
True Right ascension
17h 11m 23s
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
16:18:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
919.155 km
Perigee altitude
891.192 km
Semi-major axis
7,283.31 km
Eccentricity
0.00192
Inclination
70.0792°
RAAN
257.8478°
Arg. of periapsis
138.3202°
True anomaly
221.79035°
Mean anomaly
221.9371°
Eccentric anomaly
221.8637°
Mean motion
3.4918 °/min
Orbital period
103.1 mins
BSTAR
0.000037247
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-05-15 09:38:55.541Z | 203.071° SW | 2026-05-15 09:42:55.541Z | 206.061° SW | 44.553° | 2026-05-15 09:48:55.541Z | 24.358° NE |
| 5 mins | 2026-05-15 11:27:55.541Z | 292.454° WNW | 2026-05-15 11:29:55.541Z | 315.314° NNW | 15.309° | 2026-05-15 11:32:55.541Z | 347.013° N |
| 9 mins | 2026-05-15 18:40:55.541Z | 350.249° N | 2026-05-15 18:44:55.541Z | 51.015° ENE | 37.863° | 2026-05-15 18:49:55.541Z | 133.751° SE |
| 6 mins | 2026-05-15 20:27:55.541Z | 290.805° WNW | 2026-05-15 20:29:55.541Z | 264.886° W | 20.976° | 2026-05-15 20:33:55.541Z | 215.197° SW |
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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