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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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 02834U 67053D 26136.86151693 .00000005 00000-0 42119-4 0 9991
2 02834 69.9723 200.1278 0010080 255.0338 104.9652 13.96187559 1776Epoch: 2026-05-16T20:40Z
TLE epoch observation values (Epoch: 2026-05-16T20:40:35.062Z)
Latitude
-0.00003°
Longitude
15.40929°
Altitude
911.241 km
Speed
7.396 km/s
True Right ascension
13h 20m 30s
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
14:37:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
912.414 km
Perigee altitude
897.731 km
Semi-major axis
7,283.21 km
Eccentricity
0.00101
Inclination
69.9723°
RAAN
200.1278°
Arg. of periapsis
255.0338°
True anomaly
105.07675°
Mean anomaly
104.9652°
Eccentric anomaly
105.02098°
Mean motion
3.49188 °/min
Orbital period
103.1 mins
BSTAR
0.000042119
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-17 07:10:15.989Z | 262.198° W | 2026-05-17 07:14:15.989Z | 307.276° NW | 20.672° | 2026-05-17 07:18:15.989Z | 354.007° N |
| 9 mins | 2026-05-17 14:26:15.989Z | 359.56° N | 2026-05-17 14:30:15.989Z | 60.335° ENE | 31.097° | 2026-05-17 14:35:15.989Z | 122.56° SE |
| 8 mins | 2026-05-17 16:12:15.989Z | 305.359° NW | 2026-05-17 16:15:15.989Z | 262.719° W | 28.803° | 2026-05-17 16:20:15.989Z | 196.005° SSW |
| 10 mins | 2026-05-18 05:28:15.989Z | 200.262° SSW | 2026-05-18 05:33:15.989Z | 52.866° ENE | 44.605° | 2026-05-18 05:38:15.989Z | 25.805° NE |
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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