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: 20 hours ago

TLE from 20 hours ago
0 ATLAS CENTAUR 2 DEB
1 00701U 63047G   25341.30005564  .00001052  00000-0  32774-3 0  9990
2 00701  30.0101  47.5148 0506325  90.4740 275.3857 13.82802051 83636
Epoch: 2025-12-07T07:12Z
TLE epoch observation values (Epoch: 2025-12-07T07:12:04.807Z)
Latitude
-0.00003°
Longitude
-136.82071°
Altitude
936.355 km
Speed
7.394 km/s
True Right ascension
03h 10m 03s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
01:36:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,329.172 km
Perigee altitude
586.305 km
Semi-major axis
7,335.875 km
Eccentricity
0.05063
Inclination
30.0101°
RAAN
47.5148°
Arg. of periapsis
90.474°
True anomaly
269.58468°
Mean anomaly
275.3857°
Eccentric anomaly
272.4874°
Mean motion
3.45434 °/min
Orbital period
104.22 mins
BSTAR
0.00032774
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