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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Edit Public Description
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: 10 hours ago
TLE from 10 hours ago
0 GGSE 2
1 01244U 65016B 25297.78408017 .00000080 00000-0 96402-4 0 9992
2 01244 70.0797 327.7673 0019296 31.0559 329.1683 13.96106148 85204Epoch: 2025-10-24T18:49Z
TLE epoch observation values (Epoch: 2025-10-24T18:49:04.526Z)
Latitude
-0.00009°
Longitude
12.07439°
Altitude
897.562 km
Speed
7.41 km/s
True Right ascension
21h 51m 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
00:31:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
919.399 km
Perigee altitude
891.291 km
Semi-major axis
7,283.482 km
Eccentricity
0.00193
Inclination
70.0797°
RAAN
327.7673°
Arg. of periapsis
31.0559°
True anomaly
329.05474°
Mean anomaly
329.1683°
Eccentric anomaly
329.11154°
Mean motion
3.49168 °/min
Orbital period
103.1 mins
BSTAR
0.000096402
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-25 05:19:34.927Z | 271.318° WNW | 2025-10-25 05:23:34.927Z | 314.618° NW | 16.678° | 2025-10-25 05:26:34.927Z | 347.633° N |
| 10 mins | 2025-10-25 12:34:34.927Z | 352.498° N | 2025-10-25 12:38:34.927Z | 49.347° ENE | 35.525° | 2025-10-25 12:44:34.927Z | 132.565° SE |
| 8 mins | 2025-10-25 14:20:34.927Z | 303.525° NW | 2025-10-25 14:24:34.927Z | 251.418° W | 23.909° | 2025-10-25 14:28:34.927Z | 205.621° SW |
| 4 mins | 2025-10-26 01:55:34.927Z | 114.245° SE | 2025-10-26 01:56:34.927Z | 103.058° ESE | 14.204° | 2025-10-26 01:59:34.927Z | 70.706° E |
| 10 mins | 2025-10-26 03:37:34.927Z | 211.556° SW | 2025-10-26 03:41:34.927Z | 271.373° WNW | 43.9° | 2025-10-26 03:47:34.927Z | 21.224° 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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