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: 7 hours ago

TLE from 7 hours ago
0 ATLAS CENTAUR 2 DEB
1   698U 63047D   26063.47046483  .00000950  00000-0  32770-3 0  9992
2   698  29.9219 157.2262 0529596 347.5537  11.2405 13.74179467 64644
Epoch: 2026-03-04T11:17Z
TLE epoch observation values (Epoch: 2026-03-04T11:17:28.161Z)
Latitude
Longitude
-174.37584°
Altitude
601.602 km
Speed
7.754 km/s
True Right ascension
10h 28m 54s
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
21:58:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,378.503 km
Perigee altitude
598.248 km
Semi-major axis
7,366.512 km
Eccentricity
0.05296
Inclination
29.9219°
RAAN
157.2262°
Arg. of periapsis
347.5537°
True anomaly
12.50525°
Mean anomaly
11.2405°
Eccentric anomaly
11.86435°
Mean motion
3.43281 °/min
Orbital period
104.87 mins
BSTAR
0.0003277
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