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: 17 hours ago

TLE from 17 hours ago
0 ATLAS CENTAUR 2 DEB
1 00701U 63047G   25242.59917318  .00004420  00000-0  14574-2 0  9999
2 00701  30.0108 214.0512 0507161 335.1196  22.5713 13.82425765 69968
Epoch: 2025-08-30T14:22Z
TLE epoch observation values (Epoch: 2025-08-30T14:22:48.562Z)
Latitude
-0.00003°
Longitude
19.31765°
Altitude
613.437 km
Speed
7.728 km/s
True Right ascension
14h 16m 12s
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
23:19:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,331.182 km
Perigee altitude
586.954 km
Semi-major axis
7,337.205 km
Eccentricity
0.05072
Inclination
30.0108°
RAAN
214.0512°
Arg. of periapsis
335.1196°
True anomaly
24.93965°
Mean anomaly
22.5713°
Eccentric anomaly
23.7412°
Mean motion
3.4534 °/min
Orbital period
104.25 mins
BSTAR
0.0014574
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