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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: 1 day ago

TLE from 1 day ago
0 GGSE 4
1 02828U 67053C   25341.12818663  .00000163  00000-0  15198-3 0  9998
2 02828  69.9702 115.5025 0005448  42.4031 317.7496 13.98036479981329
Epoch: 2025-12-07T03:04Z
TLE epoch observation values (Epoch: 2025-12-07T03:04:35.324Z)
Latitude
-0.00001°
Longitude
-6.79071°
Altitude
899.98 km
Speed
7.404 km/s
True Right ascension
07h 42m 00s
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
01:37:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
902.611 km
Perigee altitude
894.682 km
Semi-major axis
7,276.784 km
Eccentricity
0.00054
Inclination
69.9702°
RAAN
115.5025°
Arg. of periapsis
42.4031°
True anomaly
317.7076°
Mean anomaly
317.7496°
Eccentric anomaly
317.7286°
Mean motion
3.4965 °/min
Orbital period
102.96 mins
BSTAR
0.00015198
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