Showing default

GGSE 4, 2828

Orbit data source: Space-Track

GGSE 4, 2828 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
2828, 1967-053C
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
NRL MULTI, Unknown motor
Mass
85 kg wet, 85 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: 16 hours ago

TLE from 16 hours ago
0 GGSE 4
1 02828U 67053C   26036.51373054  .00000113  00000-0  11712-3 0  9996
2 02828  69.9732 345.7888 0009154 321.9890  38.0569 13.98056469989763
Epoch: 2026-02-05T12:19Z
TLE epoch observation values (Epoch: 2026-02-05T12:19:46.318Z)
Latitude
-0.00009°
Longitude
25.1809°
Altitude
897.601 km
Speed
7.406 km/s
True Right ascension
23h 03m 09s
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
06:37:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
905.238 km
Perigee altitude
891.916 km
Semi-major axis
7,276.714 km
Eccentricity
0.00092
Inclination
69.9732°
RAAN
345.7888°
Arg. of periapsis
321.989°
True anomaly
38.12162°
Mean anomaly
38.0569°
Eccentric anomaly
38.08925°
Mean motion
3.49655 °/min
Orbital period
102.96 mins
BSTAR
0.00011712
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
|