TITAN 3C TRANSTAGE DEB, 1915
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 1915 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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1915 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: 9 hours ago
TLE from 9 hours ago
0 TITAN 3C TRANSTAGE DEB
1 1915U 65082FZ 26112.12028522 .00000371 00000-0 69246-4 0 9993
2 1915 31.8767 262.5743 0028570 131.1062 229.2050 14.58437040207235Epoch: 2026-04-22T02:53Z
TLE epoch observation values (Epoch: 2026-04-22T02:53:12.643Z)
Latitude
0.00002°
Longitude
9.08538°
Altitude
710.091 km
Speed
7.496 km/s
True Right ascension
17h 30m 17s
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
19:10:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
722.079 km
Perigee altitude
681.624 km
Semi-major axis
7,079.988 km
Eccentricity
0.00286
Inclination
31.8767°
RAAN
262.5743°
Arg. of periapsis
131.1062°
True anomaly
228.95773°
Mean anomaly
229.205°
Eccentric anomaly
229.08131°
Mean motion
3.6433 °/min
Orbital period
98.81 mins
BSTAR
0.000069246
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-22 14:40:32.465Z | 206.781° SW | 2026-04-22 14:42:32.465Z | 174.434° S | 23.155° | 2026-04-22 14:46:32.465Z | 115.066° SE |
| 6 mins | 2026-04-22 16:24:32.465Z | 228.812° WSW | 2026-04-22 16:26:32.465Z | 193.472° SSW | 27.426° | 2026-04-22 16:30:32.465Z | 124.948° SE |
| 6 mins | 2026-04-22 18:08:32.465Z | 235.053° WSW | 2026-04-22 18:11:32.465Z | 188.076° SSW | 20.266° | 2026-04-22 18:14:32.465Z | 148.66° 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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