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 (58 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 ATLAS CENTAUR R/B
1 03598U 68110B   26305.65130395  .00000235  00000-0  54463-4 0  9995
2 03598  34.9929  49.1908 0046939 329.1845  30.6097 14.57773829 44643
Epoch: 2026-11-01T15:37Z
TLE epoch observation values (Epoch: 2026-11-01T15:37:52.661Z)
Latitude
-0.00001°
Longitude
133.78174°
Altitude
670.76 km
Speed
7.539 km/s
True Right ascension
03h 16m 45s
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
03:42:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
736.77 km
Perigee altitude
670.289 km
Semi-major axis
7,081.666 km
Eccentricity
0.00469
Inclination
34.9929°
RAAN
49.1908°
Arg. of periapsis
329.1845°
True anomaly
30.88497°
Mean anomaly
30.6097°
Eccentric anomaly
30.7472°
Mean motion
3.642 °/min
Orbital period
98.85 mins
BSTAR
0.000054463
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Other satellites on launch #110 in the year 1968 (1968-12-07 UTC)

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