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: 12 hours ago

TLE from 12 hours ago
0 ATLAS CENTAUR 2 DEB
1 00700U 63047F   26039.10830782  .00000324  00000-0  98137-4 0  9997
2 00700  30.4807 312.4664 0717265 155.8431 207.7577 13.40154869 32801
Epoch: 2026-02-08T02:35Z
TLE epoch observation values (Epoch: 2026-02-08T02:35:57.795Z)
Latitude
-0.00006°
Longitude
135.25328°
Altitude
1,589.986 km
Speed
6.845 km/s
True Right ascension
20h 49m 51s
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
16:44:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,649.615 km
Perigee altitude
575.082 km
Semi-major axis
7,490.486 km
Eccentricity
0.07173
Inclination
30.4807°
RAAN
312.4664°
Arg. of periapsis
155.8431°
True anomaly
204.21408°
Mean anomaly
207.7577°
Eccentric anomaly
205.95881°
Mean motion
3.34794 °/min
Orbital period
107.53 mins
BSTAR
0.000098137
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