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 (63 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
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 2 weeks ago

TLE from 2 weeks ago
0 ATLAS CENTAUR 2 DEB
1 19638U 63047S   26152.52260703  .00002698  00000-0  77120-2 0  9992
2 19638  31.0053 299.5561 0627541 167.4423 257.9657 12.55671704572687
Epoch: 2026-06-01T12:32Z
TLE epoch observation values (Epoch: 2026-06-01T12:32:33.247Z)
Latitude
26.157°
Longitude
-84.17576°
Altitude
1,570.94 km
Speed
7.027 km/s
True Right ascension
23h 35m 53s
True Declination
26° 02' 06"
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
13:27:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,935.166 km
Perigee altitude
953.389 km
Semi-major axis
7,822.415 km
Eccentricity
0.06275
Inclination
31.0053°
RAAN
299.5561°
Arg. of periapsis
167.4423°
True anomaly
251.0626°
Mean anomaly
257.9657°
Eccentric anomaly
254.50091°
Mean motion
3.13713 °/min
Orbital period
114.75 mins
BSTAR
0.007712
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