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: 23 hours ago

TLE from 23 hours ago
0 ATLAS CENTAUR 2 DEB
1 02886U 63047K   26130.80617188  .00000081  00000-0  11376-4 0  9996
2 02886  29.8771  10.8935 0643454 308.5277  45.9282 13.29978270871233
Epoch: 2026-05-10T19:20Z
TLE epoch observation values (Epoch: 2026-05-10T19:20:53.250Z)
Latitude
-0.00002°
Longitude
-147.93239°
Altitude
825.87 km
Speed
7.598 km/s
True Right ascension
00h 43m 34s
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
02:52:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,634.985 km
Perigee altitude
666.112 km
Semi-major axis
7,528.685 km
Eccentricity
0.06435
Inclination
29.8771°
RAAN
10.8935°
Arg. of periapsis
308.5277°
True anomaly
51.52993°
Mean anomaly
45.9282°
Eccentric anomaly
48.69781°
Mean motion
3.3225 °/min
Orbital period
108.35 mins
BSTAR
0.000011376

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