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 shape, 0.7 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 ATLAS CENTAUR 2 DEB
1   700U 63047F   25312.54693696  .00000768  00000-0  26788-3 0  9993
2   700  30.4805  46.6623 0717495 161.1527 201.7102 13.40032237 20518
Epoch: 2025-11-08T13:07Z
TLE epoch observation values (Epoch: 2025-11-08T13:07:35.353Z)
Latitude
-0°
Longitude
161.79°
Altitude
1,611.502 km
Speed
6.825 km/s
True Right ascension
03h 06m 38s
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
11:19:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,650.276 km
Perigee altitude
575.334 km
Semi-major axis
7,490.942 km
Eccentricity
0.07175
Inclination
30.4805°
RAAN
46.6623°
Arg. of periapsis
161.1527°
True anomaly
198.9045°
Mean anomaly
201.7102°
Eccentric anomaly
200.28498°
Mean motion
3.34764 °/min
Orbital period
107.54 mins
BSTAR
0.00026788
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