Showing default

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.

Loading next visibility...
Identifier
2834, 1967-053D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
NRL MULTI, Unknown motor
Mass
105 kg wet, 105 kg dry
Launch date (UTC)
1967-05-31 (59 years ago)
Launch vehicle
THOR SLV-2 AGENA D
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 GGSE 5
1 02834U 67053D   26173.54222298  .00000000  00000-0  38753-4 0  9991
2 02834  69.9721 121.5859 0008838 218.7374 141.3099 13.96191855  6891
Epoch: 2026-06-22T13:00Z
TLE epoch observation values (Epoch: 2026-06-22T13:00:48.065Z)
Latitude
Longitude
15.65898°
Altitude
914.351 km
Speed
7.393 km/s
True Right ascension
08h 06m 20s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
02:24:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
911.495 km
Perigee altitude
898.621 km
Semi-major axis
7,283.195 km
Eccentricity
0.00088
Inclination
69.9721°
RAAN
121.5859°
Arg. of periapsis
218.7374°
True anomaly
141.37315°
Mean anomaly
141.3099°
Eccentric anomaly
141.34153°
Mean motion
3.49189 °/min
Orbital period
103.1 mins
BSTAR
0.000038753
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|