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: 1 day ago

TLE from 1 day ago
0 ATLAS CENTAUR 2 DEB
1   700U 63047F   26088.12673990  .00000186  00000-0  43116-4 0  9992
2   700  30.4812  69.2700 0717301 178.5167 181.7739 13.40172037 39382
Epoch: 2026-03-29T03:02Z
TLE epoch observation values (Epoch: 2026-03-29T03:02:30.327Z)
Latitude
0.00002°
Longitude
-162.89343°
Altitude
1,643.877 km
Speed
6.795 km/s
True Right ascension
04h 37m 04s
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
12:53:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,649.573 km
Perigee altitude
574.996 km
Semi-major axis
7,490.422 km
Eccentricity
0.07173
Inclination
30.4812°
RAAN
69.27°
Arg. of periapsis
178.5167°
True anomaly
181.54045°
Mean anomaly
181.7739°
Eccentric anomaly
181.65519°
Mean motion
3.34799 °/min
Orbital period
107.53 mins
BSTAR
0.000043116
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