ATLAS CENTAUR 2 DEB, 739

Orbit data source: Space-Track

ATLAS CENTAUR 2 DEB, 739 is space debris in LEO originally from a launch on Wed, 27 Nov 1963 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
739, 1963-047H
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
GD/Convair
Mission
Spacecraft
Bus & Motor
CENTAUR PART, Unknown motor
Mass
Unknown
Launch date (UTC)
1963-11-27 (62 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.3 m
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 ATLAS CENTAUR 2 DEB
1 00739U 63047H   25305.50621922  .00000716  00000-0  10182-3 0  9990
2 00739  30.4267 232.8258 0636928 280.2683  72.6734 13.84952337109796
Epoch: 2025-11-01T12:08Z
TLE epoch observation values (Epoch: 2025-11-01T12:08:57.340Z)
Latitude
-0.00005°
Longitude
9.55147°
Altitude
833.796 km
Speed
7.494 km/s
True Right ascension
15h 31m 18s
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
13:08:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,416.858 km
Perigee altitude
483.346 km
Semi-major axis
7,328.239 km
Eccentricity
0.06369
Inclination
30.4267°
RAAN
232.8258°
Arg. of periapsis
280.2683°
True anomaly
79.79151°
Mean anomaly
72.6734°
Eccentric anomaly
76.21766°
Mean motion
3.45974 °/min
Orbital period
104.05 mins
BSTAR
0.00010182
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