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
Last TLE update
14 hours ago
Origin
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

TLE from 14 hours ago
0 ATLAS CENTAUR 2 DEB
1 02886U 63047K   25200.78329189  .00000246  00000-0  11851-3 0  9991
2 02886  29.8742  14.6476 0643595 172.3418 188.7535 13.29881760831930
Epoch: 2025-07-19T18:47Z
TLE epoch observation values (Epoch: 2025-07-19T18:47:56.419Z)
Latitude
-0°
Longitude
154.84707°
Altitude
1,624.96 km
Speed
6.833 km/s
True Right ascension
00h 58m 35s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-20.99526°
Longitude
110.29061°
Altitude
1,491.961 km
Speed
6.956 km/s
Apparent Right ascension
22h 20m 24s
Apparent Declination
-70° 16' 25"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
21:50:17
Azimuth
177.296° S
Elevation
-20.326°
Doppler factor
1
Orbital elements
Apogee altitude
1,635.479 km
Perigee altitude
666.347 km
Semi-major axis
7,529.05 km
Eccentricity
0.06436
Inclination
29.8742°
RAAN
14.6476°
Arg. of periapsis
172.3418°
True anomaly
187.71408°
Mean anomaly
188.7535°
Eccentric anomaly
188.2259°
Mean motion
3.32225 °/min
Orbital period
108.36 mins
BSTAR
0.00011851
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