ATLAS CENTAUR 2 DEB, 701

Orbit data source: Space-Track

ATLAS CENTAUR 2 DEB, 701 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
701, 1963-047G
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, 0.5 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 00701U 63047G   26173.41683301  .00000599  00000-0  17232-3 0  9994
2 00701  30.0126  75.2328 0503912 320.0098  36.4393 13.83304825110941
Epoch: 2026-06-22T10:00Z
TLE epoch observation values (Epoch: 2026-06-22T10:00:14.372Z)
Latitude
-0.00002°
Longitude
14.56983°
Altitude
660.587 km
Speed
7.676 km/s
True Right ascension
05h 00m 55s
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
10:36:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,325.536 km
Perigee altitude
586.388 km
Semi-major axis
7,334.099 km
Eccentricity
0.05039
Inclination
30.0126°
RAAN
75.2328°
Arg. of periapsis
320.0098°
True anomaly
40.04939°
Mean anomaly
36.4393°
Eccentric anomaly
38.22579°
Mean motion
3.4556 °/min
Orbital period
104.18 mins
BSTAR
0.00017232
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