ATLAS CENTAUR 2 DEB, 700

Orbit data source: Space-Track

ATLAS CENTAUR 2 DEB, 700 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
700, 1963-047F
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
0.510 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 ATLAS CENTAUR 2 DEB
1 00700U 63047F   25260.17039073  .00000184  00000-0  49473-4 0  9996
2 00700  30.4792 306.4527 0717997 112.3806 255.4414 13.39992720 13488
Epoch: 2025-09-17T04:05Z
TLE epoch observation values (Epoch: 2025-09-17T04:05:21.759Z)
Latitude
-0°
Longitude
-111.23815°
Altitude
1,278.071 km
Speed
7.137 km/s
True Right ascension
20h 25m 48s
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
01:25:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,650.81 km
Perigee altitude
575.094 km
Semi-major axis
7,491.089 km
Eccentricity
0.0718
Inclination
30.4792°
RAAN
306.4527°
Arg. of periapsis
112.3806°
True anomaly
247.67754°
Mean anomaly
255.4414°
Eccentric anomaly
251.53927°
Mean motion
3.34754 °/min
Orbital period
107.54 mins
BSTAR
0.000049473
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