TITAN 3C TRANSTAGE DEB, 1722
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 1722 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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1722 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, 0.2 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 TITAN 3C TRANSTAGE DEB
1 1722U 65082CD 26124.60233483 .00000626 00000-0 11095-3 0 9990
2 1722 32.4173 212.2267 0026959 118.1704 242.1674 14.64006396192613Epoch: 2026-05-04T14:27Z
TLE epoch observation values (Epoch: 2026-05-04T14:27:21.729Z)
Latitude
-0.00001°
Longitude
132.89698°
Altitude
687.866 km
Speed
7.51 km/s
True Right ascension
14h 08m 54s
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
16:33:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
702.861 km
Perigee altitude
664.784 km
Semi-major axis
7,061.96 km
Eccentricity
0.0027
Inclination
32.4173°
RAAN
212.2267°
Arg. of periapsis
118.1704°
True anomaly
241.89464°
Mean anomaly
242.1674°
Eccentric anomaly
242.03098°
Mean motion
3.65726 °/min
Orbital period
98.43 mins
BSTAR
0.00011095
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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 | 2026-05-05 10:23:20.705Z | 205.659° SW | 2026-05-05 10:25:20.705Z | 169.667° S | 24.237° | 2026-05-05 10:29:20.705Z | 111.5° ESE |
| 7 mins | 2026-05-05 12:06:20.705Z | 234.6° WSW | 2026-05-05 12:09:20.705Z | 176.737° S | 28.67° | 2026-05-05 12:13:20.705Z | 119.112° SE |
| 6 mins | 2026-05-05 13:50:20.705Z | 235.43° WSW | 2026-05-05 13:52:20.705Z | 204.817° SW | 20.695° | 2026-05-05 13:56:20.705Z | 147.033° 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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