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: 13 hours ago
TLE from 13 hours ago
0 GGSE 5
1 02834U 67053D 25305.63159718 .00000021 00000-0 53999-4 0 9995
2 02834 69.9721 260.2907 0006148 167.5502 192.5756 13.96151579974376Epoch: 2025-11-01T15:09Z
TLE epoch observation values (Epoch: 2025-11-01T15:09:29.996Z)
Latitude
-0.00007°
Longitude
-8.24321°
Altitude
913.835 km
Speed
7.393 km/s
True Right ascension
17h 21m 09s
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
23:48:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
909.676 km
Perigee altitude
900.72 km
Semi-major axis
7,283.335 km
Eccentricity
0.00061
Inclination
69.9721°
RAAN
260.2907°
Arg. of periapsis
167.5502°
True anomaly
192.56027°
Mean anomaly
192.5756°
Eccentric anomaly
192.56794°
Mean motion
3.49179 °/min
Orbital period
103.1 mins
BSTAR
0.000053999
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-02 07:11:02.949Z | 357.646° N | 2025-11-02 07:16:02.949Z | 65.061° ENE | 27.377° | 2025-11-02 07:20:02.949Z | 113.383° SE |
| 9 mins | 2025-11-02 08:57:02.949Z | 314.676° NW | 2025-11-02 09:01:02.949Z | 257.848° W | 32.713° | 2025-11-02 09:06:02.949Z | 188.77° SSW |
| 10 mins | 2025-11-02 22:14:02.949Z | 192.646° SSW | 2025-11-02 22:19:02.949Z | 74.992° E | 42.897° | 2025-11-02 22:24:02.949Z | 29.098° NE |
| 6 mins | 2025-11-03 00:02:02.949Z | 277.86° WNW | 2025-11-03 00:05:02.949Z | 314.209° NW | 18.552° | 2025-11-03 00:08:02.949Z | 348.393° N |
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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