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 (62 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.5 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 00701U 63047G   26126.79527691  .00000536  00000-0  14861-3 0  9998
2 00701  30.0150 324.1901 0504557 285.0616  69.4690 13.83264632104482
Epoch: 2026-05-06T19:05Z
TLE epoch observation values (Epoch: 2026-05-06T19:05:11.925Z)
Latitude
-0.00002°
Longitude
173.23974°
Altitude
837.929 km
Speed
7.493 km/s
True Right ascension
21h 36m 45s
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
14:41:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,326.158 km
Perigee altitude
586.049 km
Semi-major axis
7,334.241 km
Eccentricity
0.05046
Inclination
30.015°
RAAN
324.1901°
Arg. of periapsis
285.0616°
True anomaly
74.9973°
Mean anomaly
69.469°
Eccentric anomaly
72.22185°
Mean motion
3.4555 °/min
Orbital period
104.18 mins
BSTAR
0.00014861
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