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: 1 day ago

TLE from 1 day ago
0 ATLAS CENTAUR 2 DEB
1 02886U 63047K   25242.07392095  .00000176  00000-0  76687-4 0  9996
2 02886  29.8697 172.5976 0643594 133.6640 231.9137 13.29894857837435
Epoch: 2025-08-30T01:46Z
TLE epoch observation values (Epoch: 2025-08-30T01:46:26.77Z)
Latitude
0.00001°
Longitude
167.47264°
Altitude
1,462.557 km
Speed
6.982 km/s
True Right ascension
11h 30m 23s
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
23:14:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,635.426 km
Perigee altitude
666.302 km
Semi-major axis
7,529.001 km
Eccentricity
0.06436
Inclination
29.8697°
RAAN
172.5976°
Arg. of periapsis
133.664°
True anomaly
226.39236°
Mean anomaly
231.9137°
Eccentric anomaly
229.1254°
Mean motion
3.32229 °/min
Orbital period
108.36 mins
BSTAR
0.000076687
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