TITAN 3C TRANSTAGE DEB, 3494
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 3494 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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3494 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: 13 hours ago
TLE from 13 hours ago
0 TITAN 3C TRANSTAGE DEB
1 03494U 65082QQ 26063.27734822 .00001126 00000-0 21144-3 0 9998
2 03494 31.8925 32.5060 0027276 248.7406 111.0321 14.61946525190081Epoch: 2026-03-04T06:39Z
TLE epoch observation values (Epoch: 2026-03-04T06:39:22.886Z)
Latitude
0.00002°
Longitude
130.6163°
Altitude
692.483 km
Speed
7.509 km/s
True Right ascension
02h 10m 01s
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
23:15:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
709.806 km
Perigee altitude
671.245 km
Semi-major axis
7,068.662 km
Eccentricity
0.00273
Inclination
31.8925°
RAAN
32.506°
Arg. of periapsis
248.7406°
True anomaly
111.32348°
Mean anomaly
111.0321°
Eccentric anomaly
111.17783°
Mean motion
3.65206 °/min
Orbital period
98.57 mins
BSTAR
0.00021144
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-05 02:36:33.768Z | 219.165° SW | 2026-03-05 02:39:33.768Z | 174.207° S | 24.971° | 2026-03-05 02:43:33.768Z | 114.71° SE |
| 7 mins | 2026-03-05 04:20:33.768Z | 237.026° WSW | 2026-03-05 04:23:33.768Z | 187.528° SSW | 28.072° | 2026-03-05 04:27:33.768Z | 125.155° SE |
| 5 mins | 2026-03-05 06:05:33.768Z | 228.325° WSW | 2026-03-05 06:07:33.768Z | 197.771° SSW | 19.593° | 2026-03-05 06:10:33.768Z | 156.37° 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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