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
Radar Cross Section
0.290 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 ATLAS CENTAUR 2 DEB
1 00739U 63047H   25242.93967361  .00000609  00000-0  89062-4 0  9992
2 00739  30.4204 207.4467 0636885 113.2226 253.6708 13.84891882101114
Epoch: 2025-08-30T22:33Z
TLE epoch observation values (Epoch: 2025-08-30T22:33:07.799Z)
Latitude
-0°
Longitude
-110.20258°
Altitude
1,102.825 km
Speed
7.224 km/s
True Right ascension
13h 49m 47s
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
23:16:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,417.054 km
Perigee altitude
483.578 km
Semi-major axis
7,328.453 km
Eccentricity
0.06369
Inclination
30.4204°
RAAN
207.4467°
Arg. of periapsis
113.2226°
True anomaly
246.83668°
Mean anomaly
253.6708°
Eccentric anomaly
250.23666°
Mean motion
3.45959 °/min
Orbital period
104.06 mins
BSTAR
0.000089062
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