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: 20 hours ago

TLE from 20 hours ago
0 ATLAS CENTAUR 2 DEB
1 00739U 63047H   26079.75801612  .00000336  00000-0  43168-4 0  9991
2 00739  30.4221 207.8714 0635698  13.6474 348.0480 13.85190864129110
Epoch: 2026-03-20T18:11Z
TLE epoch observation values (Epoch: 2026-03-20T18:11:32.592Z)
Latitude
-0.00002°
Longitude
116.69708°
Altitude
490.099 km
Speed
7.854 km/s
True Right ascension
13h 51m 29s
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
19:06:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,415.063 km
Perigee altitude
483.461 km
Semi-major axis
7,327.399 km
Eccentricity
0.06357
Inclination
30.4221°
RAAN
207.8714°
Arg. of periapsis
13.6474°
True anomaly
346.41296°
Mean anomaly
348.048°
Eccentric anomaly
347.24377°
Mean motion
3.46034 °/min
Orbital period
104.04 mins
BSTAR
0.000043168
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