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   25241.43517299  .00007852  00000-0  21894-1 0  9998
2 19638  31.0073  27.9136 0646342 145.8360 255.2833 12.55009320537968
Epoch: 2025-08-29T10:26Z
TLE epoch observation values (Epoch: 2025-08-29T10:26:38.946Z)
Latitude
16.85233°
Longitude
-76.52898°
Altitude
1,599.841 km
Speed
7.001 km/s
True Right ascension
03h 52m 04s
True Declination
16° 46' 02"
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
23:16:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,952.802 km
Perigee altitude
941.255 km
Semi-major axis
7,825.166 km
Eccentricity
0.06463
Inclination
31.0073°
RAAN
27.9136°
Arg. of periapsis
145.836°
True anomaly
248.28135°
Mean anomaly
255.2833°
Eccentric anomaly
251.76599°
Mean motion
3.13547 °/min
Orbital period
114.82 mins
BSTAR
0.021894
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