TITAN 3C TRANSTAGE R/B, 3432
Orbit data source: Space-Track
TITAN 3C TRANSTAGE R/B, 3432 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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3432 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 TITAN 3C TRANSTAGE R/B
1 03432U 68081E 25347.31916162 .00000071 00000-0 00000-0 0 9993
2 03432 1.5928 44.2523 0095066 278.8927 35.5411 1.01514615120093Epoch: 2025-12-13T07:39Z
TLE epoch observation values (Epoch: 2025-12-13T07:39:35.563Z)
Latitude
-1.11858°
Longitude
162.1849°
Altitude
35,120.747 km
Speed
3.111 km/s
True Right ascension
23h 57m 19s
True Declination
-1° 07' 03"
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
01:35:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,840.397 km
Perigee altitude
35,045.247 km
Semi-major axis
41,820.959 km
Eccentricity
0.00951
Inclination
1.5928°
RAAN
44.2523°
Arg. of periapsis
278.8927°
True anomaly
36.18051°
Mean anomaly
35.5411°
Eccentric anomaly
35.86018°
Mean motion
0.25378 °/min
Orbital period
1,418.57 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 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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3432 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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