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 shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 20 hours ago

TLE from 20 hours ago
0 ATLAS CENTAUR 2 DEB
1 03741U 63047L   26134.59356438  .00001941  00000-0  35648-3 0  9998
2 03741  29.8767 213.1850 0237491  14.2931 346.4250 14.46155937907939
Epoch: 2026-05-14T14:14Z
TLE epoch observation values (Epoch: 2026-05-14T14:14:43.962Z)
Latitude
0.00001°
Longitude
127.16483°
Altitude
572.663 km
Speed
7.664 km/s
True Right ascension
14h 12m 44s
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
19:07:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
911.226 km
Perigee altitude
573.026 km
Semi-major axis
7,120.263 km
Eccentricity
0.02375
Inclination
29.8767°
RAAN
213.185°
Arg. of periapsis
14.2931°
True anomaly
345.76728°
Mean anomaly
346.425°
Eccentric anomaly
346.09807°
Mean motion
3.61243 °/min
Orbital period
99.66 mins
BSTAR
0.00035648
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