TITAN 3C TRANSTAGE R/B, 4632
Orbit data source: Space-Track
TITAN 3C TRANSTAGE R/B, 4632 is space debris originally from a launch on Fri, 06 Nov 1970 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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4632 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 TITAN 3C TRANSTAGE R/B
1 04632U 70093B 26170.92544351 -.00000157 00000-0 00000-0 0 9997
2 04632 15.1334 35.8275 1369388 277.9084 74.7068 1.20232144142445Epoch: 2026-06-19T22:12Z
TLE epoch observation values (Epoch: 2026-06-19T22:12:38.319Z)
Latitude
2.16117°
Longitude
162.53252°
Altitude
30,332.368 km
Speed
3.324 km/s
True Right ascension
02h 55m 21s
True Declination
2° 09' 31"
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
23:08:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,097.326 km
Perigee altitude
25,865.397 km
Semi-major axis
37,359.499 km
Eccentricity
0.13694
Inclination
15.1334°
RAAN
35.8275°
Arg. of periapsis
277.9084°
True anomaly
90.35941°
Mean anomaly
74.7068°
Eccentric anomaly
82.48543°
Mean motion
0.30057 °/min
Orbital period
1,197.74 mins
BSTAR
0
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Other satellites on launch #93 in the year 1970 (1970-11-06 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. |
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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