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 days ago

TLE from 2 days ago
0 ATLAS CENTAUR 2 DEB
1 19638U 63047S   26173.36386330  .00003991  00000-0  11318-1 0  9995
2 19638  31.0111 211.4285 0631625 305.0041 155.1061 12.55845963575302
Epoch: 2026-06-22T08:43Z
TLE epoch observation values (Epoch: 2026-06-22T08:43:57.789Z)
Latitude
30.25285°
Longitude
-85.08084°
Altitude
1,892.664 km
Speed
6.744 km/s
True Right ascension
21h 05m 50s
True Declination
30° 07' 26"
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
10:41:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,937.592 km
Perigee altitude
949.517 km
Semi-major axis
7,821.691 km
Eccentricity
0.06316
Inclination
31.0111°
RAAN
211.4285°
Arg. of periapsis
305.0041°
True anomaly
157.94755°
Mean anomaly
155.1061°
Eccentric anomaly
156.54646°
Mean motion
3.13756 °/min
Orbital period
114.74 mins
BSTAR
0.011318
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