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: 6 hours ago

TLE from 6 hours ago
0 ATLAS CENTAUR 2 DEB
1  2886U 63047K   25302.50391781  .00000129  00000-0  37094-4 0  9999
2  2886  29.8751 236.8869 0643790 243.9812 109.3096 13.29906399845486
Epoch: 2025-10-29T12:05Z
TLE epoch observation values (Epoch: 2025-10-29T12:05:38.498Z)
Latitude
0.00001°
Longitude
17.4004°
Altitude
1,332.636 km
Speed
7.104 km/s
True Right ascension
15h 47m 32s
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
13:41:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,635.526 km
Perigee altitude
666.113 km
Semi-major axis
7,528.957 km
Eccentricity
0.06438
Inclination
29.8751°
RAAN
236.8869°
Arg. of periapsis
243.9812°
True anomaly
116.07553°
Mean anomaly
109.3096°
Eccentric anomaly
112.71221°
Mean motion
3.32232 °/min
Orbital period
108.36 mins
BSTAR
0.000037094
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