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  2886U 63047K   26030.96607888  .00000346  00000-0  18175-3 0  9995
2  2886  29.8744 139.5128 0643500 251.4411 101.5228 13.29955853857936
Epoch: 2026-01-30T23:11Z
TLE epoch observation values (Epoch: 2026-01-30T23:11:09.215Z)
Latitude
-0.00002°
Longitude
21.52753°
Altitude
1,271.418 km
Speed
7.161 km/s
True Right ascension
09h 18m 03s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
23:41:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,635.11 km
Perigee altitude
666.157 km
Semi-major axis
7,528.77 km
Eccentricity
0.06435
Inclination
29.8744°
RAAN
139.5128°
Arg. of periapsis
251.4411°
True anomaly
108.61569°
Mean anomaly
101.5228°
Eccentric anomaly
105.08277°
Mean motion
3.32244 °/min
Orbital period
108.35 mins
BSTAR
0.00018175
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