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 (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: 2 days ago

TLE from 2 days ago
0 ATLAS CENTAUR 2 DEB
1 00739U 63047H   26173.37585419  .00000679  00000-0  10167-3 0  9990
2 00739  30.4225  66.9300 0635258  82.6739 284.5564 13.85288786142103
Epoch: 2026-06-22T09:01Z
TLE epoch observation values (Epoch: 2026-06-22T09:01:13.802Z)
Latitude
0.00003°
Longitude
21.05988°
Altitude
855.101 km
Speed
7.472 km/s
True Right ascension
04h 27m 43s
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
10:39:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.374 km
Perigee altitude
483.46 km
Semi-major axis
7,327.054 km
Eccentricity
0.06353
Inclination
30.4225°
RAAN
66.93°
Arg. of periapsis
82.6739°
True anomaly
277.38599°
Mean anomaly
284.5564°
Eccentric anomaly
280.98331°
Mean motion
3.46058 °/min
Orbital period
104.03 mins
BSTAR
0.00010167

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