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  2886U 63047K   26088.01842028  .00000105  00000-0  30634-4 0  9999
2  2886  29.8726 220.3034 0643269 335.4876  21.6350 13.29974757865538
Epoch: 2026-03-29T00:26Z
TLE epoch observation values (Epoch: 2026-03-29T00:26:31.512Z)
Latitude
0.00002°
Longitude
27.2418°
Altitude
700.181 km
Speed
7.726 km/s
True Right ascension
14h 41m 12s
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
12:55:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,634.86 km
Perigee altitude
666.264 km
Semi-major axis
7,528.699 km
Eccentricity
0.06433
Inclination
29.8726°
RAAN
220.3034°
Arg. of periapsis
335.4876°
True anomaly
24.57022°
Mean anomaly
21.635°
Eccentric anomaly
23.07983°
Mean motion
3.32249 °/min
Orbital period
108.35 mins
BSTAR
0.000030634
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