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: 1 day ago

TLE from 1 day ago
0 ATLAS CENTAUR 2 DEB
1  3741U 63047L   26079.29405640  .00007268  00000-0  14045-2 0  9998
2  3741  29.8781 179.7859 0238740 214.8853 143.5888 14.45370459899929
Epoch: 2026-03-20T07:03Z
TLE epoch observation values (Epoch: 2026-03-20T07:03:26.472Z)
Latitude
-0.00003°
Longitude
-103.90563°
Altitude
877.383 km
Speed
7.344 km/s
True Right ascension
11h 59m 08s
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
19:06:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
914.753 km
Perigee altitude
574.652 km
Semi-major axis
7,122.839 km
Eccentricity
0.02387
Inclination
29.8781°
RAAN
179.7859°
Arg. of periapsis
214.8853°
True anomaly
145.17436°
Mean anomaly
143.5888°
Eccentric anomaly
144.38536°
Mean motion
3.61047 °/min
Orbital period
99.71 mins
BSTAR
0.0014045
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