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: 14 hours ago

TLE from 14 hours ago
0 ATLAS CENTAUR 2 DEB
1  2886U 63047K   26041.25119677  .00000296  00000-0  15740-3 0  9992
2  2886  29.8740  89.1808 0643521 331.4746  25.1998 13.29962347859304
Epoch: 2026-02-10T06:01Z
TLE epoch observation values (Epoch: 2026-02-10T06:01:43.400Z)
Latitude
-0.00001°
Longitude
-141.5844°
Altitude
713.556 km
Speed
7.713 km/s
True Right ascension
05h 56m 43s
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
22:31:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,635.099 km
Perigee altitude
666.118 km
Semi-major axis
7,528.746 km
Eccentricity
0.06435
Inclination
29.874°
RAAN
89.1808°
Arg. of periapsis
331.4746°
True anomaly
28.58319°
Mean anomaly
25.1998°
Eccentric anomaly
26.86602°
Mean motion
3.32246 °/min
Orbital period
108.35 mins
BSTAR
0.0001574
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