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: 14 hours ago

TLE from 14 hours ago
0 ATLAS CENTAUR 2 DEB
1   701U 63047G   26306.77198396  .00000331  00000-0  86170-4 0  9998
2   701  30.0100  82.9622 0503391  10.1056 350.9237 13.83517208129422
Epoch: 2026-11-02T18:31Z
TLE epoch observation values (Epoch: 2026-11-02T18:31:39.414Z)
Latitude
-0.00003°
Longitude
123.00372°
Altitude
586.18 km
Speed
7.755 km/s
True Right ascension
05h 31m 50s
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
04:16:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,324.367 km
Perigee altitude
586.058 km
Semi-major axis
7,333.349 km
Eccentricity
0.05034
Inclination
30.01°
RAAN
82.9622°
Arg. of periapsis
10.1056°
True anomaly
349.95366°
Mean anomaly
350.9237°
Eccentric anomaly
350.44493°
Mean motion
3.45613 °/min
Orbital period
104.16 mins
BSTAR
0.00008617
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