TITAN 3C TRANSTAGE DEB, 1961
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 1961 is 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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1961 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 TITAN 3C TRANSTAGE DEB
1 01961U 65082GW 26139.20325944 .00003851 00000-0 19248-3 0 9992
2 01961 31.8549 113.6303 0003313 310.5381 49.4985 15.15916519239755Epoch: 2026-05-19T04:52Z
TLE epoch observation values (Epoch: 2026-05-19T04:52:41.615Z)
Latitude
-0.00006°
Longitude
163.57627°
Altitude
515.304 km
Speed
7.609 km/s
True Right ascension
07h 34m 31s
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
05:24:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
524.207 km
Perigee altitude
519.635 km
Semi-major axis
6,900.058 km
Eccentricity
0.00033
Inclination
31.8549°
RAAN
113.6303°
Arg. of periapsis
310.5381°
True anomaly
49.52738°
Mean anomaly
49.4985°
Eccentric anomaly
49.51294°
Mean motion
3.78673 °/min
Orbital period
95.07 mins
BSTAR
0.00019248
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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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-20 03:19:16.608Z | 205.29° SW | 2026-05-20 03:21:16.608Z | 162.682° S | 20.701° | 2026-05-20 03:23:16.608Z | 127.264° SE |
| 4 mins | 2026-05-20 04:59:16.608Z | 220.417° SW | 2026-05-20 05:01:16.608Z | 176.295° S | 21.58° | 2026-05-20 05:03:16.608Z | 140.243° SSE |
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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