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: 9 hours ago

TLE from 9 hours ago
0 ATLAS CENTAUR 2 DEB
1   739U 63047H   25336.35846296  .00001443  00000-0  22531-3 0  9999
2   739  30.4240  67.7979 0636299 180.2158 179.8215 13.85012772114071
Epoch: 2025-12-02T08:36Z
TLE epoch observation values (Epoch: 2025-12-02T08:36:11.199Z)
Latitude
-0.00002°
Longitude
-132.69356°
Altitude
1,410.615 km
Speed
6.926 km/s
True Right ascension
04h 31m 11s
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
15:08:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,416.171 km
Perigee altitude
483.608 km
Semi-major axis
7,328.026 km
Eccentricity
0.06363
Inclination
30.424°
RAAN
67.7979°
Arg. of periapsis
180.2158°
True anomaly
179.84254°
Mean anomaly
179.8215°
Eccentric anomaly
179.83218°
Mean motion
3.45989 °/min
Orbital period
104.05 mins
BSTAR
0.00022531
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