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, 0.089 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 ATLAS CENTAUR 2 DEB
1 19638U 63047S   26301.60700108 -.00007307  00000-0 -19461-1 0  9992
2 19638  31.0107  27.8264 0656312  67.2189  60.4195 12.56778756591448
Epoch: 2026-10-28T14:34Z
TLE epoch observation values (Epoch: 2026-10-28T14:34:04.893Z)
Latitude
21.66966°
Longitude
-88.76711°
Altitude
1,208.267 km
Speed
7.358 km/s
True Right ascension
11h 06m 49s
True Declination
21° 33' 32"
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
18:06:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,952.782 km
Perigee altitude
926.595 km
Semi-major axis
7,817.826 km
Eccentricity
0.06563
Inclination
31.0107°
RAAN
27.8264°
Arg. of periapsis
67.2189°
True anomaly
67.21954°
Mean anomaly
60.4195°
Eccentric anomaly
63.79335°
Mean motion
3.13989 °/min
Orbital period
114.65 mins
BSTAR
-0.019461
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