ATLAS CENTAUR 2 DEB, 701

Orbit data source: Space-Track

ATLAS CENTAUR 2 DEB, 701 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
701, 1963-047G
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
GD/Convair
Mission
Spacecraft
Bus & Motor
CENTAUR PART, Unknown motor
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, 0.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 ATLAS CENTAUR 2 DEB
1 00701U 63047G   26301.57587273  .00000298  00000-0  72340-4 0  9993
2 00701  30.0091 110.7191 0503487 326.0709  30.8617 13.83514175128708
Epoch: 2026-10-28T13:49Z
TLE epoch observation values (Epoch: 2026-10-28T13:49:15.403Z)
Latitude
-0.00004°
Longitude
-133.51782°
Altitude
638.472 km
Speed
7.699 km/s
True Right ascension
07h 22m 52s
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
16:51:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,324.448 km
Perigee altitude
585.998 km
Semi-major axis
7,333.36 km
Eccentricity
0.05035
Inclination
30.0091°
RAAN
110.7191°
Arg. of periapsis
326.0709°
True anomaly
33.98833°
Mean anomaly
30.8617°
Eccentric anomaly
32.40777°
Mean motion
3.45612 °/min
Orbital period
104.16 mins
BSTAR
0.00007234
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