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: 17 hours ago

TLE from 17 hours ago
0 ATLAS CENTAUR 2 DEB
1 00701U 63047G   26036.50456871  .00002931  00000-0  94914-3 0  9996
2 00701  30.0135  86.2415 0504712 240.2587 114.6864 13.82989761 91975
Epoch: 2026-02-05T12:06Z
TLE epoch observation values (Epoch: 2026-02-05T12:06:34.736Z)
Latitude
-0.00002°
Longitude
128.94089°
Altitude
1,121.216 km
Speed
7.21 km/s
True Right ascension
05h 44m 57s
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
07:37:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,327.291 km
Perigee altitude
586.858 km
Semi-major axis
7,335.212 km
Eccentricity
0.05047
Inclination
30.0135°
RAAN
86.2415°
Arg. of periapsis
240.2587°
True anomaly
119.79958°
Mean anomaly
114.6864°
Eccentric anomaly
117.25708°
Mean motion
3.45481 °/min
Orbital period
104.2 mins
BSTAR
0.00094914
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