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: 1 day ago
TLE from 1 day ago
0 TITAN 3C TRANSTAGE DEB
1 33512U 68081N 26087.10631886 .00000005 00000-0 00000+0 0 9997
2 33512 1.8771 41.9077 0258417 306.9719 51.0531 1.00900546 72818Epoch: 2026-03-28T02:33Z
TLE epoch observation values (Epoch: 2026-03-28T02:33:05.949Z)
Latitude
0°
Longitude
178.50528°
Altitude
34,942.375 km
Speed
3.131 km/s
True Right ascension
02h 49m 14s
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
12:31:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,697.425 km
Perigee altitude
34,527.216 km
Semi-major axis
41,990.457 km
Eccentricity
0.02584
Inclination
1.8771°
RAAN
41.9077°
Arg. of periapsis
306.9719°
True anomaly
53.40317°
Mean anomaly
51.0531°
Eccentric anomaly
52.22339°
Mean motion
0.25224 °/min
Orbital period
1,427.2 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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