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: 11 hours ago
TLE from 11 hours ago
0 GGSE 5
1 02834U 67053D 25310.86160474 .00000024 00000-0 56209-4 0 9997
2 02834 69.9724 249.0925 0005836 159.8262 200.3075 13.96152554975102Epoch: 2025-11-06T20:40Z
TLE epoch observation values (Epoch: 2025-11-06T20:40:42.649Z)
Latitude
-0.00005°
Longitude
-107.39907°
Altitude
913.448 km
Speed
7.394 km/s
True Right ascension
16h 36m 22s
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
04:01:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
909.445 km
Perigee altitude
900.944 km
Semi-major axis
7,283.332 km
Eccentricity
0.00058
Inclination
69.9724°
RAAN
249.0925°
Arg. of periapsis
159.8262°
True anomaly
200.28431°
Mean anomaly
200.3075°
Eccentric anomaly
200.2959°
Mean motion
3.49179 °/min
Orbital period
103.1 mins
BSTAR
0.000056209
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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 | 2025-11-07 20:51:57.133Z | 178.572° S | 2025-11-07 20:56:57.133Z | 100.582° ESE | 37.253° | 2025-11-07 21:01:57.133Z | 36.588° NE |
| 8 mins | 2025-11-07 22:38:57.133Z | 259.428° W | 2025-11-07 22:42:57.133Z | 312.612° NW | 24.019° | 2025-11-07 22:46:57.133Z | 359.298° N |
| 8 mins | 2025-11-08 05:54:57.133Z | 6.633° NNE | 2025-11-08 05:57:57.133Z | 47.868° ENE | 26.57° | 2025-11-08 06:02:57.133Z | 112.489° ESE |
| 9 mins | 2025-11-08 07:39:57.133Z | 315.382° NNW | 2025-11-08 07:43:57.133Z | 255.829° W | 33.884° | 2025-11-08 07:48:57.133Z | 186.627° SSW |
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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