ATLAS CENTAUR R/B, 3598

Orbit data source: Space-Track

ATLAS CENTAUR R/B, 3598 is space debris in LEO originally from a launch on Sat, 07 Dec 1968 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
3598, 1968-110B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
GD/Convair
Mission
Spacecraft
Bus & Motor
CENTAUR D, Unknown motor
Mass
~1,700 kg wet, ~1,700 kg dry
Launch date (UTC)
1968-12-07 (57 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 ATLAS CENTAUR R/B
1  3598U 68110B   25294.93151284  .00001166  00000-0  25478-3 0  9999
2  3598  34.9935  22.0568 0046412 146.2797 214.0863 14.57308573989852
Epoch: 2025-10-21T22:21Z
TLE epoch observation values (Epoch: 2025-10-21T22:21:22.709Z)
Latitude
0.00001°
Longitude
16.09981°
Altitude
728.072 km
Speed
7.479 km/s
True Right ascension
01h 28m 13s
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
02:25:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
737.909 km
Perigee altitude
672.161 km
Semi-major axis
7,083.172 km
Eccentricity
0.00464
Inclination
34.9935°
RAAN
22.0568°
Arg. of periapsis
146.2797°
True anomaly
213.78966°
Mean anomaly
214.0863°
Eccentric anomaly
213.93784°
Mean motion
3.64084 °/min
Orbital period
98.88 mins
BSTAR
0.00025478
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Other satellites on launch #110 in the year 1968 (1968-12-07 UTC)

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