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: 14 hours ago

TLE from 14 hours ago
0 ATLAS CENTAUR 2 DEB
1 19638U 63047S   26031.27912126  .00003521  00000-0  85321-2 0  9991
2 19638  31.0105  92.5598 0691070  85.8561 335.8804 12.56371322557430
Epoch: 2026-01-31T06:41Z
TLE epoch observation values (Epoch: 2026-01-31T06:41:56.076Z)
Latitude
26.08737°
Longitude
-84.31128°
Altitude
950.899 km
Speed
7.606 km/s
True Right ascension
09h 46m 42s
True Declination
25° 57' 19"
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
22:11:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,981.763 km
Perigee altitude
900.996 km
Semi-major axis
7,819.517 km
Eccentricity
0.06911
Inclination
31.0105°
RAAN
92.5598°
Arg. of periapsis
85.8561°
True anomaly
332.37062°
Mean anomaly
335.8804°
Eccentric anomaly
334.15424°
Mean motion
3.13887 °/min
Orbital period
114.69 mins
BSTAR
0.0085321
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