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: 8 hours ago
TLE from 8 hours ago
0 GGSE 2
1 01244U 65016B 26035.30907873 .00000065 00000-0 85068-4 0 9994
2 01244 70.0790 109.3798 0023846 264.0772 95.7616 13.96136031 99515Epoch: 2026-02-04T07:25Z
TLE epoch observation values (Epoch: 2026-02-04T07:25:04.402Z)
Latitude
-0.00004°
Longitude
-136.36607°
Altitude
911.309 km
Speed
7.396 km/s
True Right ascension
07h 17m 31s
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
17:31:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
922.609 km
Perigee altitude
887.873 km
Semi-major axis
7,283.378 km
Eccentricity
0.00238
Inclination
70.079°
RAAN
109.3798°
Arg. of periapsis
264.0772°
True anomaly
96.03339°
Mean anomaly
95.7616°
Eccentric anomaly
95.8975°
Mean motion
3.49176 °/min
Orbital period
103.1 mins
BSTAR
0.000085068
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Other satellites on launch #16 in the year 1965 (1965-03-09 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-02-04 16:35:34.476Z | 323.037° NNW | 2026-02-04 16:40:34.476Z | 264.555° W | 35.941° | 2026-02-04 16:46:34.476Z | 180.812° SSW |
| 10 mins | 2026-02-05 05:53:34.476Z | 186.84° SSW | 2026-02-05 05:58:34.476Z | 89.312° E | 41.322° | 2026-02-05 06:03:34.476Z | 31.746° NE |
| 7 mins | 2026-02-05 07:41:34.476Z | 274.804° WNW | 2026-02-05 07:44:34.476Z | 313.474° NW | 20.727° | 2026-02-05 07:48:34.476Z | 357.052° N |
| 9 mins | 2026-02-05 14:55:34.476Z | 355.814° N | 2026-02-05 15:00:34.476Z | 68.063° E | 30.626° | 2026-02-05 15:04:34.476Z | 118.753° SE |
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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