GGSE 5, 2834
Orbit data source: Space-Track
GGSE 5, 2834 is an American payload satellite in LEO that was launched on Wed, 31 May 1967 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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2834 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
NRL MULTI, Unknown motor
Mass
105 kg wet, 105 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: 9 hours ago
TLE from 9 hours ago
0 GGSE 5
1 2834U 67053D 25295.74472345 .00000041 00000-0 68864-4 0 9998
2 2834 69.9713 281.4614 0006788 181.1070 179.0022 13.96149607972990Epoch: 2025-10-22T17:52Z
TLE epoch observation values (Epoch: 2025-10-22T17:52:24.106Z)
Latitude
0.00003°
Longitude
-18.05296°
Altitude
914.415 km
Speed
7.393 km/s
True Right ascension
18h 45m 50s
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
21:41:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
910.149 km
Perigee altitude
900.261 km
Semi-major axis
7,283.342 km
Eccentricity
0.00068
Inclination
69.9713°
RAAN
281.4614°
Arg. of periapsis
181.107°
True anomaly
179.00355°
Mean anomaly
179.0022°
Eccentric anomaly
179.00288°
Mean motion
3.49178 °/min
Orbital period
103.1 mins
BSTAR
0.000068864
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Other satellites on launch #53 in the year 1967 (1967-05-31 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 5 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-23 02:42:06.618Z | 292.674° NW | 2025-10-23 02:44:06.618Z | 313.677° NW | 13.47° | 2025-10-23 02:47:06.618Z | 344.465° N |
| 10 mins | 2025-10-23 09:55:06.618Z | 345.129° N | 2025-10-23 10:00:06.618Z | 87.194° E | 40.866° | 2025-10-23 10:05:06.618Z | 142.828° SSE |
| 6 mins | 2025-10-23 11:42:06.618Z | 289.74° WNW | 2025-10-23 11:45:06.618Z | 253.623° W | 17.764° | 2025-10-23 11:48:06.618Z | 221.117° SW |
| 7 mins | 2025-10-23 23:14:06.618Z | 138.918° SSE | 2025-10-23 23:17:06.618Z | 103.52° ESE | 19.775° | 2025-10-23 23:21:06.618Z | 58.079° ENE |
| 10 mins | 2025-10-24 00:58:06.618Z | 224.542° SW | 2025-10-24 01:02:06.618Z | 286.219° WNW | 39.74° | 2025-10-24 01:08:06.618Z | 16.475° 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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