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: 17 hours ago

TLE from 17 hours ago
0 ATLAS CENTAUR 2 DEB
1 19638U 63047S   25340.15514341  .00005511  00000-0  13481-1 0  9995
2 19638  31.0128 330.3553 0692979  77.8860 359.3392 12.55691962550374
Epoch: 2025-12-06T03:43Z
TLE epoch observation values (Epoch: 2025-12-06T03:43:24.390Z)
Latitude
30.28235°
Longitude
-85.62826°
Altitude
898.697 km
Speed
7.659 km/s
True Right ascension
03h 01m 38s
True Declination
30° 08' 09"
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
18:27:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,986.269 km
Perigee altitude
902.126 km
Semi-major axis
7,822.334 km
Eccentricity
0.0693
Inclination
31.0128°
RAAN
330.3553°
Arg. of periapsis
77.886°
True anomaly
359.23897°
Mean anomaly
359.3392°
Eccentric anomaly
359.29°
Mean motion
3.13717 °/min
Orbital period
114.75 mins
BSTAR
0.013481
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