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: 17 hours ago

TLE from 17 hours ago
0 ATLAS CENTAUR 2 DEB
1   700U 63047F   25299.88198675  .00000463  00000-0  15913-3 0  9991
2   700  30.4771 109.4838 0717615  62.2938 304.8585 13.40018684 18817
Epoch: 2025-10-26T21:10Z
TLE epoch observation values (Epoch: 2025-10-26T21:10:03.655Z)
Latitude
-0.00001°
Longitude
116.47674°
Altitude
828.313 km
Speed
7.578 km/s
True Right ascension
07h 17m 56s
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
10:02:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,650.421 km
Perigee altitude
575.291 km
Semi-major axis
7,490.993 km
Eccentricity
0.07176
Inclination
30.4771°
RAAN
109.4838°
Arg. of periapsis
62.2938°
True anomaly
297.76524°
Mean anomaly
304.8585°
Eccentric anomaly
301.34704°
Mean motion
3.3476 °/min
Orbital period
107.54 mins
BSTAR
0.00015913
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