TITAN 3C TRANSTAGE DEB, 33512
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 33512 is space debris in GEO originally from a launch on Thu, 26 Sep 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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33512 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 TITAN 3C TRANSTAGE DEB
1 33512U 68081N 26313.07682545 -.00000213 00000-0 00000-0 0 9996
2 33512 2.3232 48.1074 0157180 277.2013 80.6077 1.00901129 75098Epoch: 2026-11-09T01:50Z
TLE epoch observation values (Epoch: 2026-11-09T01:50:37.718Z)
Latitude
0°
Longitude
-28.25375°
Altitude
35,511.663 km
Speed
3.088 km/s
True Right ascension
03h 10m 38s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
21:35:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,272.161 km
Perigee altitude
34,952.154 km
Semi-major axis
41,990.294 km
Eccentricity
0.01572
Inclination
2.3232°
RAAN
48.1074°
Arg. of periapsis
277.2013°
True anomaly
82.39013°
Mean anomaly
80.6077°
Eccentric anomaly
81.49838°
Mean motion
0.25224 °/min
Orbital period
1,427.19 mins
BSTAR
0
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Other satellites on launch #81 in the year 1968 (1968-09-26 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.TITAN 3C TRANSTAGE DEB Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| TITAN 3C TRANSTAGE DEB is likely not visible in the next few days. |
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33512 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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