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.

Not visible in the next 10 days
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 (63 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: 6 hours ago

TLE from 6 hours ago
0 ATLAS CENTAUR 2 DEB
1 00739U 63047H   26301.57586333  .00000307  00000-0  39118-4 0  9997
2 00739  30.4206 100.8356 0634845  83.3069 283.9323 13.85363911159890
Epoch: 2026-10-28T13:49Z
TLE epoch observation values (Epoch: 2026-10-28T13:49:14.591Z)
Latitude
0.00001°
Longitude
-143.39785°
Altitude
859.913 km
Speed
7.467 km/s
True Right ascension
06h 43m 20s
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
15:25:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.79 km
Perigee altitude
483.515 km
Semi-major axis
7,326.79 km
Eccentricity
0.06348
Inclination
30.4206°
RAAN
100.8356°
Arg. of periapsis
83.3069°
True anomaly
276.75298°
Mean anomaly
283.9323°
Eccentric anomaly
280.35414°
Mean motion
3.46077 °/min
Orbital period
104.02 mins
BSTAR
0.000039118
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