ATLAS CENTAUR 2 DEB, 2886

Orbit data source: Space-Track

ATLAS CENTAUR 2 DEB, 2886 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
2886, 1963-047K
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
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, 0.2 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 ATLAS CENTAUR 2 DEB
1 02886U 63047K   25315.71750885  .00000248  00000-0  12759-3 0  9992
2 02886  29.8712 172.2284 0643478 346.8010  11.6422 13.29910173847242
Epoch: 2025-11-11T17:13Z
TLE epoch observation values (Epoch: 2025-11-11T17:13:12.764Z)
Latitude
-0.00003°
Longitude
-137.17489°
Altitude
672.872 km
Speed
7.755 km/s
True Right ascension
11h 28m 54s
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
14:47:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,635.277 km
Perigee altitude
666.335 km
Semi-major axis
7,528.943 km
Eccentricity
0.06435
Inclination
29.8712°
RAAN
172.2284°
Arg. of periapsis
346.801°
True anomaly
13.25676°
Mean anomaly
11.6422°
Eccentric anomaly
12.43617°
Mean motion
3.32233 °/min
Orbital period
108.36 mins
BSTAR
0.00012759
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