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 (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: 2 days ago

TLE from 2 days ago
0 ATLAS CENTAUR 2 DEB
1 00698U 63047D   26152.02586415  .00001346  00000-0  47828-3 0  9996
2 00698  29.9230  50.8896 0528500   8.5615 352.3589 13.74270015 76830
Epoch: 2026-06-01T00:37Z
TLE epoch observation values (Epoch: 2026-06-01T00:37:14.662Z)
Latitude
-0.00003°
Longitude
152.05935°
Altitude
597.617 km
Speed
7.758 km/s
True Right ascension
03h 23m 33s
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
16:01:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,377.355 km
Perigee altitude
598.749 km
Semi-major axis
7,366.189 km
Eccentricity
0.05285
Inclination
29.923°
RAAN
50.8896°
Arg. of periapsis
8.5615°
True anomaly
351.49741°
Mean anomaly
352.3589°
Eccentric anomaly
351.93402°
Mean motion
3.43304 °/min
Orbital period
104.86 mins
BSTAR
0.00047828
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