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   26031.32494821  .00000900  00000-0  13496-3 0  9999
2   739  30.4254 107.0053 0636056 325.4775  30.6036 13.85145982122395
Epoch: 2026-01-31T07:47Z
TLE epoch observation values (Epoch: 2026-01-31T07:47:55.525Z)
Latitude
-0.00006°
Longitude
-140.52672°
Altitude
551.734 km
Speed
7.788 km/s
True Right ascension
07h 08m 01s
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
20:25:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,415.493 km
Perigee altitude
483.346 km
Semi-major axis
7,327.557 km
Eccentricity
0.06361
Inclination
30.4254°
RAAN
107.0053°
Arg. of periapsis
325.4775°
True anomaly
34.5827°
Mean anomaly
30.6036°
Eccentric anomaly
32.56519°
Mean motion
3.46023 °/min
Orbital period
104.04 mins
BSTAR
0.00013496
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