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 03598U 68110B   26125.92174645  .00000431  00000-0  96233-4 0  9990
2 03598  34.9939 349.6473 0047234 303.2331  56.3841 14.57633021 18407
Epoch: 2026-05-05T22:07Z
TLE epoch observation values (Epoch: 2026-05-05T22:07:18.893Z)
Latitude
-0.00003°
Longitude
154.02889°
Altitude
681.368 km
Speed
7.528 km/s
True Right ascension
23h 18m 35s
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
14:51:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
737.436 km
Perigee altitude
670.533 km
Semi-major axis
7,082.122 km
Eccentricity
0.00472
Inclination
34.9939°
RAAN
349.6473°
Arg. of periapsis
303.2331°
True anomaly
56.83632°
Mean anomaly
56.3841°
Eccentric anomaly
56.61006°
Mean motion
3.64165 °/min
Orbital period
98.86 mins
BSTAR
0.000096233
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Other satellites on launch #110 in the year 1968 (1968-12-07 UTC)

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