ATLAS CENTAUR 2 DEB, 3741

Orbit data source: Space-Track

ATLAS CENTAUR 2 DEB, 3741 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
3741, 1963-047L
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: 21 hours ago

TLE from 21 hours ago
0 ATLAS CENTAUR 2 DEB
1 03741U 63047L   25242.44284274  .00005606  00000-0  11405-2 0  9995
2 03741  29.8779 287.4638 0252672 126.2786 236.1432 14.41344880870736
Epoch: 2025-08-30T10:37Z
TLE epoch observation values (Epoch: 2025-08-30T10:37:41.612Z)
Latitude
-0.00003°
Longitude
149.1633°
Altitude
855.953 km
Speed
7.373 km/s
True Right ascension
19h 09m 51s
True Declination
0° 00' 00"
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
23:19:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
938.253 km
Perigee altitude
577.636 km
Semi-major axis
7,136.082 km
Eccentricity
0.02527
Inclination
29.8779°
RAAN
287.4638°
Arg. of periapsis
126.2786°
True anomaly
233.78103°
Mean anomaly
236.1432°
Eccentric anomaly
234.95792°
Mean motion
3.60042 °/min
Orbital period
99.99 mins
BSTAR
0.0011405
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