SATCOM 3 DEB, 29004

Orbit data source: Space-Track

SATCOM 3 DEB, 29004 is space debris in HEO originally from a launch on Fri, 07 Dec 1979 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
29004, 1979-101G
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1979-12-07 (46 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 SATCOM 3 DEB
1 29004U 79101G   25263.26725598 -.00000164  00000-0  00000-0 0  9997
2 29004   8.1946 113.9773 4868563  47.4860 119.0924  1.81236200129860
Epoch: 2025-09-20T06:24Z
TLE epoch observation values (Epoch: 2025-09-20T06:24:50.916Z)
Latitude
-3.04741°
Longitude
-139.81013°
Altitude
32,304.533 km
Speed
2.566 km/s
True Right ascension
21h 03m 13s
True Declination
-3° 02' 39"
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
13:48:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,876.619 km
Perigee altitude
8,204.82 km
Semi-major axis
28,418.857 km
Eccentricity
0.48686
Inclination
8.1946°
RAAN
113.9773°
Arg. of periapsis
47.486°
True anomaly
154.46958°
Mean anomaly
119.0924°
Eccentric anomaly
137.82199°
Mean motion
0.45304 °/min
Orbital period
794.64 mins
BSTAR
0
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