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 (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: 1 day ago

TLE from 1 day ago
0 ATLAS CENTAUR 2 DEB
1 03741U 63047L   26173.72735817  .00002782  00000-0  51802-3 0  9992
2 03741  29.8790 341.9140 0236436  21.8703 339.1803 14.46379042913605
Epoch: 2026-06-22T17:27Z
TLE epoch observation values (Epoch: 2026-06-22T17:27:23.745Z)
Latitude
-0.00003°
Longitude
169.15589°
Altitude
579.252 km
Speed
7.656 km/s
True Right ascension
22h 47m 39s
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
10:37:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
909.726 km
Perigee altitude
573.063 km
Semi-major axis
7,119.531 km
Eccentricity
0.02364
Inclination
29.879°
RAAN
341.914°
Arg. of periapsis
21.8703°
True anomaly
338.19004°
Mean anomaly
339.1803°
Eccentric anomaly
338.68795°
Mean motion
3.61298 °/min
Orbital period
99.64 mins
BSTAR
0.00051802
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