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
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   25258.30792211  .00004622  00000-0  12478-1 0  9991
2 19638  31.0112 316.6300 0656730 258.4024 169.4235 12.55121372540084
Epoch: 2025-09-15T07:23Z
TLE epoch observation values (Epoch: 2025-09-15T07:23:24.47Z)
Latitude
28.8795°
Longitude
-82.76543°
Altitude
1,948.362 km
Speed
6.697 km/s
True Right ascension
01h 30m 24s
True Declination
28° 45' 18"
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
01:20:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,960.435 km
Perigee altitude
932.692 km
Semi-major axis
7,824.7 km
Eccentricity
0.06567
Inclination
31.0112°
RAAN
316.63°
Arg. of periapsis
258.4024°
True anomaly
170.70128°
Mean anomaly
169.4235°
Eccentric anomaly
170.07223°
Mean motion
3.13575 °/min
Orbital period
114.81 mins
BSTAR
0.012478
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