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: 1 day ago

TLE from 1 day ago
0 ATLAS CENTAUR 2 DEB
1 00698U 63047D   26300.42246604  .00000381  00000-0  11077-3 0  9993
2 00698  29.9220 349.2160 0528009 170.6513 190.4349 13.74450144 97268
Epoch: 2026-10-27T10:08Z
TLE epoch observation values (Epoch: 2026-10-27T10:08:21.065Z)
Latitude
-0.00002°
Longitude
161.34237°
Altitude
1,364.941 km
Speed
6.99 km/s
True Right ascension
23h 16m 51s
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
16:49:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,376.316 km
Perigee altitude
598.501 km
Semi-major axis
7,365.546 km
Eccentricity
0.0528
Inclination
29.922°
RAAN
349.216°
Arg. of periapsis
170.6513°
True anomaly
189.40604°
Mean anomaly
190.4349°
Eccentric anomaly
189.91404°
Mean motion
3.43349 °/min
Orbital period
104.85 mins
BSTAR
0.00011077
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