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: 10 hours ago

TLE from 10 hours ago
0 ATLAS CENTAUR 2 DEB
1 00701U 63047G   25286.86211390  .00001500  00000-0  47632-3 0  9992
2 00701  30.0126 337.9639 0506802 349.7025   9.3505 13.82674154 76098
Epoch: 2025-10-13T20:41Z
TLE epoch observation values (Epoch: 2025-10-13T20:41:26.640Z)
Latitude
-0.00005°
Longitude
4.944°
Altitude
586.87 km
Speed
7.755 km/s
True Right ascension
22h 31m 51s
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
01:35:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,329.996 km
Perigee altitude
586.383 km
Semi-major axis
7,336.327 km
Eccentricity
0.05068
Inclination
30.0126°
RAAN
337.9639°
Arg. of periapsis
349.7025°
True anomaly
10.35675°
Mean anomaly
9.3505°
Eccentric anomaly
9.8471°
Mean motion
3.45402 °/min
Orbital period
104.23 mins
BSTAR
0.00047632
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