TITAN 3C TRANSTAGE DEB, 2789 (Decayed)
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 2789 was space debris in LEO originally from a launch on Fri, 15 Oct 1965 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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2789 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 TITAN 3C TRANSTAGE DEB
1 02789U 65082KR 25318.16751908 .01423176 00000-0 75203-2 0 9996
2 02789 32.2566 351.0947 0021342 141.4725 218.7483 15.76572341 48744Epoch: 2025-11-14T04:01Z
TLE epoch observation values (Epoch: 2025-11-14T04:01:13.648Z)
Latitude
0°
Longitude
-122.72707°
Altitude
349.946 km
Speed
7.695 km/s
True Right ascension
23h 24m 22s
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
06:30:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
358.267 km
Perigee altitude
329.575 km
Semi-major axis
6,722.058 km
Eccentricity
0.00213
Inclination
32.2566°
RAAN
351.0947°
Arg. of periapsis
141.4725°
True anomaly
218.59555°
Mean anomaly
218.7483°
Eccentric anomaly
218.67189°
Mean motion
3.93813 °/min
Orbital period
91.41 mins
BSTAR
0.0075203
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Other satellites on launch #82 in the year 1965 (1965-10-15 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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| This satellite is decayed. |
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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