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 shape, 0.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 ATLAS CENTAUR 2 DEB
1   701U 63047G   25311.84269997  .00001287  00000-0  39900-3 0  9996
2   701  30.0110 204.6898 0506639 201.1507 156.7414 13.82742074 79559
Epoch: 2025-11-07T20:13Z
TLE epoch observation values (Epoch: 2025-11-07T20:13:29.277Z)
Latitude
Longitude
-145.96304°
Altitude
1,296.617 km
Speed
7.039 km/s
True Right ascension
13h 38m 45s
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
01:38:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,329.625 km
Perigee altitude
586.275 km
Semi-major axis
7,336.087 km
Eccentricity
0.05066
Inclination
30.011°
RAAN
204.6898°
Arg. of periapsis
201.1507°
True anomaly
158.90713°
Mean anomaly
156.7414°
Eccentric anomaly
157.83649°
Mean motion
3.45419 °/min
Orbital period
104.22 mins
BSTAR
0.000399
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