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
Defense Technology
Bus & Motor
NRL MULTI, Unknown motor
Mass
105 kg wet, 105 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Ell + 2 Ant, 9.0 m
Radar Cross Section
1.247 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 GGSE 5
1 02834U 67053D 25261.21219054 -.00000004 00000-0 35793-4 0 9994
2 02834 69.9756 355.4001 0008815 219.7100 140.3362 13.96142265968170Epoch: 2025-09-18T05:05Z
TLE epoch observation values (Epoch: 2025-09-18T05:05:33.262Z)
Latitude
0.00006°
Longitude
-78.3655°
Altitude
914.442 km
Speed
7.393 km/s
True Right ascension
23h 41m 36s
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
13:32:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
911.65 km
Perigee altitude
898.81 km
Semi-major axis
7,283.367 km
Eccentricity
0.00088
Inclination
69.9756°
RAAN
355.4001°
Arg. of periapsis
219.71°
True anomaly
140.40062°
Mean anomaly
140.3362°
Eccentric anomaly
140.36842°
Mean motion
3.49176 °/min
Orbital period
103.1 mins
BSTAR
0.000035793
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-09-19 06:59:10.186Z | 172.95° S | 2025-09-19 07:04:10.186Z | 115.634° SE | 32.315° | 2025-09-19 07:09:10.186Z | 43.353° NE |
| 9 mins | 2025-09-19 08:46:10.186Z | 249.145° W | 2025-09-19 08:50:10.186Z | 303.388° NW | 28.162° | 2025-09-19 08:55:10.186Z | 5.116° NNE |
| 8 mins | 2025-09-19 16:02:10.186Z | 5.259° NNE | 2025-09-19 16:06:10.186Z | 55.424° ENE | 22.976° | 2025-09-19 16:10:10.186Z | 102.739° ESE |
| 10 mins | 2025-09-19 17:47:10.186Z | 323.239° NNW | 2025-09-19 17:52:10.186Z | 241.872° WSW | 38.591° | 2025-09-19 17:57:10.186Z | 177.298° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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