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
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 ATLAS CENTAUR 2 DEB
1 02886U 63047K   25259.18758289  .00000135  00000-0  42341-4 0  9992
2 02886  29.8752  88.8525 0643745 266.8688  85.8082 13.29898965839717
Epoch: 2025-09-16T04:30Z
TLE epoch observation values (Epoch: 2025-09-16T04:30:07.161Z)
Latitude
-0.00003°
Longitude
25.94113°
Altitude
1,141.407 km
Speed
7.286 km/s
True Right ascension
05h 55m 24s
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
12:08:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,635.522 km
Perigee altitude
666.173 km
Semi-major axis
7,528.985 km
Eccentricity
0.06437
Inclination
29.8752°
RAAN
88.8525°
Arg. of periapsis
266.8688°
True anomaly
93.18829°
Mean anomaly
85.8082°
Eccentric anomaly
89.49644°
Mean motion
3.3223 °/min
Orbital period
108.36 mins
BSTAR
0.000042341
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