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 (63 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: 1 day ago

TLE from 1 day ago
0 ATLAS CENTAUR 2 DEB
1 00700U 63047F   26173.50039132  .00000412  00000-0  13518-3 0  9997
2 00700  30.4802   5.7080 0716841 125.0073 241.9927 13.40213783 50844
Epoch: 2026-06-22T12:00Z
TLE epoch observation values (Epoch: 2026-06-22T12:00:33.810Z)
Latitude
-0.00002°
Longitude
-85.11832°
Altitude
1,387.474 km
Speed
7.033 km/s
True Right ascension
00h 22m 49s
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
10:36:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,649.062 km
Perigee altitude
575.196 km
Semi-major axis
7,490.266 km
Eccentricity
0.07168
Inclination
30.4802°
RAAN
5.708°
Arg. of periapsis
125.0073°
True anomaly
235.05052°
Mean anomaly
241.9927°
Eccentric anomaly
238.49107°
Mean motion
3.34809 °/min
Orbital period
107.52 mins
BSTAR
0.00013518
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