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: 14 hours ago

TLE from 14 hours ago
0 ATLAS CENTAUR 2 DEB
1  3741U 63047L   26031.28016108  .00004995  00000-0  96965-3 0  9998
2  3741  29.8777 102.9033 0242682 124.4787 237.8988 14.44484173892972
Epoch: 2026-01-31T06:43Z
TLE epoch observation values (Epoch: 2026-01-31T06:43:25.917Z)
Latitude
Longitude
-128.4611°
Altitude
836.942 km
Speed
7.387 km/s
True Right ascension
06h 51m 36s
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
22:09:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
920.542 km
Perigee altitude
574.683 km
Semi-major axis
7,125.75 km
Eccentricity
0.02427
Inclination
29.8777°
RAAN
102.9033°
Arg. of periapsis
124.4787°
True anomaly
235.58107°
Mean anomaly
237.8988°
Eccentric anomaly
236.73616°
Mean motion
3.60826 °/min
Orbital period
99.77 mins
BSTAR
0.00096965
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