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: 18 hours ago

TLE from 18 hours ago
0 ATLAS CENTAUR 2 DEB
1 19638U 63047S   26035.17143229  .00003856  00000-0  94090-2 0  9998
2 19638  31.0121  76.0628 0688116 111.2833 301.1005 12.56404426557927
Epoch: 2026-02-04T04:06Z
TLE epoch observation values (Epoch: 2026-02-04T04:06:51.749Z)
Latitude
21.58297°
Longitude
-79.09845°
Altitude
1,187.072 km
Speed
7.378 km/s
True Right ascension
07h 47m 50s
True Declination
21° 28' 20"
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
23:58:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,979.306 km
Perigee altitude
903.178 km
Semi-major axis
7,819.379 km
Eccentricity
0.06881
Inclination
31.0121°
RAAN
76.0628°
Arg. of periapsis
111.2833°
True anomaly
294.05327°
Mean anomaly
301.1005°
Eccentric anomaly
297.60676°
Mean motion
3.13895 °/min
Orbital period
114.69 mins
BSTAR
0.009409
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