TITAN 3C TRANSTAGE DEB, 39297
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 39297 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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39297 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 39297U 68081AH 26311.46952803 -.00000031 00000-0 00000-0 0 9998
2 39297 1.8124 33.1768 0207955 297.7630 59.6080 1.00389149 17919Epoch: 2026-11-07T11:16Z
TLE epoch observation values (Epoch: 2026-11-07T11:16:07.221Z)
Latitude
-0.00002°
Longitude
176.88608°
Altitude
35,322.17 km
Speed
3.108 km/s
True Right ascension
02h 10m 21s
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
19:44:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,630.971 km
Perigee altitude
34,878.621 km
Semi-major axis
42,132.933 km
Eccentricity
0.0208
Inclination
1.8124°
RAAN
33.1768°
Arg. of periapsis
297.763°
True anomaly
61.69045°
Mean anomaly
59.608°
Eccentric anomaly
60.64652°
Mean motion
0.25096 °/min
Orbital period
1,434.47 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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39297 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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