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: 11 hours ago

TLE from 11 hours ago
0 ATLAS CENTAUR 2 DEB
1   739U 63047H   26121.34198968  .00000652  00000-0  95780-4 0  9995
2   739  30.4256 345.3689 0635593   4.0870 356.4614 13.85218869134883
Epoch: 2026-05-01T08:12Z
TLE epoch observation values (Epoch: 2026-05-01T08:12:27.908Z)
Latitude
-0.00004°
Longitude
2.97692°
Altitude
479.611 km
Speed
7.866 km/s
True Right ascension
23h 01m 28s
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
02:56:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.881 km
Perigee altitude
483.445 km
Semi-major axis
7,327.3 km
Eccentricity
0.06356
Inclination
30.4256°
RAAN
345.3689°
Arg. of periapsis
4.087°
True anomaly
355.9733°
Mean anomaly
356.4614°
Eccentric anomaly
356.22141°
Mean motion
3.46041 °/min
Orbital period
104.03 mins
BSTAR
0.00009578
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