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 (63 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
Medium (>0.1 m² and <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   26300.23130733  .00000087  00000-0  10933-4 0  9992
2 02886  29.8726 261.6860 0643245 187.3722 171.6981 13.30011314893801
Epoch: 2026-10-27T05:33Z
TLE epoch observation values (Epoch: 2026-10-27T05:33:04.953Z)
Latitude
0.00001°
Longitude
142.81797°
Altitude
1,624.673 km
Speed
6.833 km/s
True Right ascension
17h 26m 44s
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
18:06:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,634.695 km
Perigee altitude
666.153 km
Semi-major axis
7,528.561 km
Eccentricity
0.06432
Inclination
29.8726°
RAAN
261.686°
Arg. of periapsis
187.3722°
True anomaly
172.68371°
Mean anomaly
171.6981°
Eccentric anomaly
172.19839°
Mean motion
3.32258 °/min
Orbital period
108.35 mins
BSTAR
0.000010933
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