ATLAS CENTAUR 2 DEB, 701

Orbit data source: Space-Track

ATLAS CENTAUR 2 DEB, 701 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
701, 1963-047G
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
Radar Cross Section
0.560 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 ATLAS CENTAUR 2 DEB
1 00701U 63047G   25256.39311417  .00001797  00000-0  57870-3 0  9991
2 00701  30.0082 140.4846 0507026  91.8637 274.0067 13.82516048 71871
Epoch: 2025-09-13T09:26Z
TLE epoch observation values (Epoch: 2025-09-13T09:26:05.064Z)
Latitude
0.00001°
Longitude
6.33639°
Altitude
946.324 km
Speed
7.384 km/s
True Right ascension
09h 21m 56s
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
21:15:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,330.748 km
Perigee altitude
586.75 km
Semi-major axis
7,336.886 km
Eccentricity
0.0507
Inclination
30.0082°
RAAN
140.4846°
Arg. of periapsis
91.8637°
True anomaly
268.19502°
Mean anomaly
274.0067°
Eccentric anomaly
271.10219°
Mean motion
3.45363 °/min
Orbital period
104.24 mins
BSTAR
0.0005787
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