TITAN 3C TRANSTAGE DEB, 43283
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 43283 is space debris in GEO originally from a launch on Sun, 09 Feb 1969 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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43283 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 TITAN 3C TRANSTAGE DEB
1 43283U 69013D 26192.20983767 -.00000091 00000-0 00000-0 0 9992
2 43283 1.5138 89.8746 0337195 144.7022 216.6267 0.93096423 28310Epoch: 2026-07-11T05:02Z
TLE epoch observation values (Epoch: 2026-07-11T05:02:09.974Z)
Latitude
-0.00001°
Longitude
84.3277°
Altitude
39,145.343 km
Speed
2.918 km/s
True Right ascension
05h 55m 58s
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
14:57:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
39,421.205 km
Perigee altitude
36,433.294 km
Semi-major axis
44,305.386 km
Eccentricity
0.03372
Inclination
1.5138°
RAAN
89.8746°
Arg. of periapsis
144.7022°
True anomaly
214.39754°
Mean anomaly
216.6267°
Eccentric anomaly
215.50466°
Mean motion
0.23273 °/min
Orbital period
1,546.84 mins
BSTAR
0
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Other satellites on launch #13 in the year 1969 (1969-02-09 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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43283 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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