TITAN 3C TRANSTAGE DEB, 39298
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 39298 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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39298 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 TITAN 3C TRANSTAGE DEB
1 39298U 68081AJ 26257.75118083 -.00000138 00000-0 00000-0 0 9992
2 39298 1.7767 31.0534 0148623 317.2665 83.0953 1.00184010 67186Epoch: 2026-09-14T18:01Z
TLE epoch observation values (Epoch: 2026-09-14T18:01:42.023Z)
Latitude
1.16966°
Longitude
168.94435°
Altitude
35,743.358 km
Speed
3.079 km/s
True Right ascension
04h 52m 23s
True Declination
1° 10' 07"
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
03:23:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,439.335 km
Perigee altitude
35,185.241 km
Semi-major axis
42,190.425 km
Eccentricity
0.01486
Inclination
1.7767°
RAAN
31.0534°
Arg. of periapsis
317.2665°
True anomaly
84.78958°
Mean anomaly
83.0953°
Eccentric anomaly
83.94209°
Mean motion
0.25045 °/min
Orbital period
1,437.41 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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39298 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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