ATLAS CENTAUR 2 DEB, 19638

Orbit data source: Space-Track

ATLAS CENTAUR 2 DEB, 19638 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
19638, 1963-047S
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, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 ATLAS CENTAUR 2 DEB
1 19638U 63047S   25293.95773551  .00005755  00000-0  14545-1 0  9992
2 19638  31.0101 165.8987 0681854 133.8613 347.3089 12.55437889544566
Epoch: 2025-10-20T22:59Z
TLE epoch observation values (Epoch: 2025-10-20T22:59:08.348Z)
Latitude
26.81385°
Longitude
-85.30002°
Altitude
922.771 km
Speed
7.635 km/s
True Right ascension
19h 16m 32s
True Declination
26° 40' 44"
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
03:32:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,978.692 km
Perigee altitude
911.81 km
Semi-major axis
7,823.388 km
Eccentricity
0.06819
Inclination
31.0101°
RAAN
165.8987°
Arg. of periapsis
133.8613°
True anomaly
345.43761°
Mean anomaly
347.3089°
Eccentric anomaly
346.38957°
Mean motion
3.13654 °/min
Orbital period
114.78 mins
BSTAR
0.014545
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