TITAN 3C TRANSTAGE R/B, 2868
Orbit data source: Space-Track
TITAN 3C TRANSTAGE R/B, 2868 is space debris in GEO originally from a launch on Sat, 01 Jul 1967 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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2868 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 TITAN 3C TRANSTAGE R/B
1 2868U 67066G 25289.11863917 -.00000086 00000-0 00000+0 0 9995
2 2868 1.7924 106.9740 0084085 161.5038 112.0547 1.08907582125676
Epoch: 2025-10-16T02:50Z
TLE epoch observation values (Epoch: 2025-10-16T02:50:50.424Z)
Latitude
-1.78466°
Longitude
-46.18881°
Altitude
33,655.383 km
Speed
3.15 km/s
True Right ascension
01h 25m 37s
True Declination
-1° 46' 58"
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
04:36:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,863.767 km
Perigee altitude
33,192.662 km
Semi-major axis
39,906.352 km
Eccentricity
0.00841
Inclination
1.7924°
RAAN
106.974°
Arg. of periapsis
161.5038°
True anomaly
112.94419°
Mean anomaly
112.0547°
Eccentric anomaly
112.4998°
Mean motion
0.27226 °/min
Orbital period
1,322.28 mins
BSTAR
0
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Other satellites on launch #66 in the year 1967 (1967-07-01 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 R/B 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 R/B is likely not visible in the next few days. |
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2868 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 ascending 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 ascending order |
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