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: 5 hours ago

TLE from 5 hours ago
0 ATLAS CENTAUR 2 DEB
1 03741U 63047L   25255.94590770  .00002747  00000-0  54634-3 0  9990
2 03741  29.8791 208.2736 0251919 252.1821 105.1146 14.41471656872687
Epoch: 2025-09-12T22:42Z
TLE epoch observation values (Epoch: 2025-09-12T22:42:06.425Z)
Latitude
0.00002°
Longitude
-124.43946°
Altitude
803.096 km
Speed
7.428 km/s
True Right ascension
13h 53m 05s
True Declination
0° 00' 00"
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
20:40:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
937.287 km
Perigee altitude
577.766 km
Semi-major axis
7,135.663 km
Eccentricity
0.02519
Inclination
29.8791°
RAAN
208.2736°
Arg. of periapsis
252.1821°
True anomaly
107.87774°
Mean anomaly
105.1146°
Eccentric anomaly
106.49856°
Mean motion
3.60074 °/min
Orbital period
99.98 mins
BSTAR
0.00054634
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