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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.

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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: 13 hours ago

TLE from 13 hours ago
0 GGSE 4
1  2828U 67053C   26130.45328118  .00000058  00000-0  78191-4 0  9998
2  2828  69.9688 143.9936 0009856 230.9149 129.1081 13.98079692  2883
Epoch: 2026-05-10T10:52Z
TLE epoch observation values (Epoch: 2026-05-10T10:52:43.493Z)
Latitude
-0.0001°
Longitude
112.5562°
Altitude
907.295 km
Speed
7.396 km/s
True Right ascension
09h 35m 58s
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
07:38:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
905.669 km
Perigee altitude
891.325 km
Semi-major axis
7,276.634 km
Eccentricity
0.00099
Inclination
69.9688°
RAAN
143.9936°
Arg. of periapsis
230.9149°
True anomaly
129.19567°
Mean anomaly
129.1081°
Eccentric anomaly
129.15189°
Mean motion
3.49661 °/min
Orbital period
102.96 mins
BSTAR
0.000078191
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