ATLAS CENTAUR 2 DEB, 698

Orbit data source: Space-Track

ATLAS CENTAUR 2 DEB, 698 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
698, 1963-047D
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: 15 hours ago

TLE from 15 hours ago
0 ATLAS CENTAUR 2 DEB
1 00698U 63047D   25293.03300479  .00000929  00000-0  31675-3 0  9995
2 00698  29.9234 150.1452 0531311 294.6731  59.9430 13.73766178 46007
Epoch: 2025-10-20T00:47Z
TLE epoch observation values (Epoch: 2025-10-20T00:47:31.613Z)
Latitude
-0.00006°
Longitude
109.52225°
Altitude
804.85 km
Speed
7.543 km/s
True Right ascension
10h 00m 34s
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
10:59:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,381.32 km
Perigee altitude
598.382 km
Semi-major axis
7,367.988 km
Eccentricity
0.05313
Inclination
29.9234°
RAAN
150.1452°
Arg. of periapsis
294.6731°
True anomaly
65.38549°
Mean anomaly
59.943°
Eccentric anomaly
62.64682°
Mean motion
3.43178 °/min
Orbital period
104.9 mins
BSTAR
0.00031675
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