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: 10 hours ago

TLE from 10 hours ago
0 GGSE 4
1 02828U 67053C   26083.87719951  .00000080  00000-0  94122-4 0  9997
2 02828  69.9694 244.0442 0010448 275.7272  84.2643 13.98068494996388
Epoch: 2026-03-24T21:03Z
TLE epoch observation values (Epoch: 2026-03-24T21:03:10.037Z)
Latitude
-0.00005°
Longitude
105.90381°
Altitude
902.052 km
Speed
7.402 km/s
True Right ascension
16h 16m 10s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
11:45:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
906.138 km
Perigee altitude
890.933 km
Semi-major axis
7,276.673 km
Eccentricity
0.00104
Inclination
69.9694°
RAAN
244.0442°
Arg. of periapsis
275.7272°
True anomaly
84.38344°
Mean anomaly
84.2643°
Eccentric anomaly
84.32387°
Mean motion
3.49658 °/min
Orbital period
102.96 mins
BSTAR
0.000094122
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
|