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 (62 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.5 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   701U 63047G   26087.89542832  .00001128  00000-0  34795-3 0  9995
2   701  30.0115 171.8993 0504616 315.5446  40.5682 13.83214800 99090
Epoch: 2026-03-28T21:29Z
TLE epoch observation values (Epoch: 2026-03-28T21:29:25.006Z)
Latitude
-0.00004°
Longitude
23.23593°
Altitude
678.447 km
Speed
7.658 km/s
True Right ascension
11h 27m 35s
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
12:53:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,326.386 km
Perigee altitude
586.174 km
Semi-major axis
7,334.417 km
Eccentricity
0.05046
Inclination
30.0115°
RAAN
171.8993°
Arg. of periapsis
315.5446°
True anomaly
44.51456°
Mean anomaly
40.5682°
Eccentric anomaly
42.52232°
Mean motion
3.45537 °/min
Orbital period
104.19 mins
BSTAR
0.00034795
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