TITAN 3C TRANSTAGE DEB, 26050
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 26050 is space debris in HEO originally from a launch on Tue, 21 Dec 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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26050 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 1 day ago
0 TITAN 3C TRANSTAGE DEB
1 26050U 65108AJ 25198.51761460 -.00000217 00000-0 -10075-1 0 9994
2 26050 26.6964 358.3685 6621015 51.8484 351.2270 2.69848914257181
Epoch: 2025-07-17T12:25Z
TLE epoch observation values (Epoch: 2025-07-17T12:25:21.901Z)
Latitude
0.00008°
Longitude
-123.5638°
Altitude
2,318.754 km
Speed
8.566 km/s
True Right ascension
23h 53m 26s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-0.29326°
Longitude
56.57004°
Altitude
14,278.895 km
Speed
4.506 km/s
Apparent Right ascension
12h 44m 46s
Apparent Declination
-10° 45' 13"
Sunlit
Visualization observer readout
Local Sidereal Time
05:16:36
Azimuth
84.14° E
Elevation
-23.735°
Doppler factor
1
Orbital elements
Apogee altitude
29,849.993 km
Perigee altitude
986.895 km
Semi-major axis
21,796.581 km
Eccentricity
0.6621
Inclination
26.6964°
RAAN
358.3685°
Arg. of periapsis
51.8484°
True anomaly
308.55203°
Mean anomaly
351.227°
Eccentric anomaly
335.48831°
Mean motion
0.67447 °/min
Orbital period
533.75 mins
BSTAR
-0.010075
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Other satellites on launch #108 in the year 1965 (1965-12-21 UTC)
TITAN 3C TRANSTAGE DEB Visibility forecast
Observer location: undefined°, undefined°
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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241 mins | 2025-07-19 00:51:07.861Z | 251.464° W | 2025-07-19 01:41:07.861Z | 220.418° SW | 21.367° | 2025-07-19 04:52:07.861Z | 214.883° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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