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   25345.44485266  .00000399  00000-0  21647-3 0  9996
2 02886  29.8761  26.7485 0643251 218.1993 137.1267 13.29922237851208
Epoch: 2025-12-11T10:40Z
TLE epoch observation values (Epoch: 2025-12-11T10:40:35.269Z)
Latitude
-0.00003°
Longitude
146.20076°
Altitude
1,513.663 km
Speed
6.935 km/s
True Right ascension
01h 46m 59s
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
17:55:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,635.057 km
Perigee altitude
666.463 km
Semi-major axis
7,528.897 km
Eccentricity
0.06433
Inclination
29.8761°
RAAN
26.7485°
Arg. of periapsis
218.1993°
True anomaly
141.85687°
Mean anomaly
137.1267°
Eccentric anomaly
139.51933°
Mean motion
3.32236 °/min
Orbital period
108.36 mins
BSTAR
0.00021647
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