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: 2 days ago

TLE from 2 days ago
0 ATLAS CENTAUR 2 DEB
1 19638U 63047S   25308.49463610  .00002525  00000-0  61942-2 0  9996
2 19638  31.0177 104.3852 0688154 229.5087 170.7763 12.55520580546397
Epoch: 2025-11-04T11:52Z
TLE epoch observation values (Epoch: 2025-11-04T11:52:16.559Z)
Latitude
20.01401°
Longitude
-80.57845°
Altitude
1,971.662 km
Speed
6.675 km/s
True Right ascension
09h 25m 53s
True Declination
19° 55' 11"
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
16:32:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,983.253 km
Perigee altitude
906.561 km
Semi-major axis
7,823.044 km
Eccentricity
0.06882
Inclination
31.0177°
RAAN
104.3852°
Arg. of periapsis
229.5087°
True anomaly
171.94101°
Mean anomaly
170.7763°
Eccentric anomaly
171.36807°
Mean motion
3.13675 °/min
Orbital period
114.77 mins
BSTAR
0.0061942
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