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: 1 week ago

TLE from 1 week ago
0 ATLAS CENTAUR 2 DEB
1 00739U 63047H   26152.40174927  .00000957  00000-0  14163-3 0  9998
2 00739  30.4250 179.1698 0635571 265.8818  86.8937 13.85258964139196
Epoch: 2026-06-01T09:38Z
TLE epoch observation values (Epoch: 2026-06-01T09:38:31.136Z)
Latitude
-0.00001°
Longitude
144.65045°
Altitude
948.167 km
Speed
7.378 km/s
True Right ascension
11h 56m 40s
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
12:00:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,414.715 km
Perigee altitude
483.329 km
Semi-major axis
7,327.159 km
Eccentricity
0.06356
Inclination
30.425°
RAAN
179.1698°
Arg. of periapsis
265.8818°
True anomaly
94.17786°
Mean anomaly
86.8937°
Eccentric anomaly
90.53509°
Mean motion
3.46051 °/min
Orbital period
104.03 mins
BSTAR
0.00014163
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