TITAN 3C TRANSTAGE DEB, 26525
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 26525 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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26525 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 TITAN 3C TRANSTAGE DEB
1 26525U 65108AL 25242.08284050 .00000193 00000-0 20106-2 0 9996
2 26525 26.4911 292.5622 6714361 167.6033 214.7304 2.83249752262460
Epoch: 2025-08-30T01:59Z
TLE epoch observation values (Epoch: 2025-08-30T01:59:17.419Z)
Latitude
-1.35133°
Longitude
-78.47618°
Altitude
27,953.44 km
Speed
2.081 km/s
True Right ascension
19h 19m 28s
True Declination
-1° 20' 59"
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
16:05:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
28,895.718 km
Perigee altitude
555.849 km
Semi-major axis
21,103.92 km
Eccentricity
0.67144
Inclination
26.4911°
RAAN
292.5622°
Arg. of periapsis
167.6033°
True anomaly
189.37956°
Mean anomaly
214.7304°
Eccentric anomaly
200.96547°
Mean motion
0.70794 °/min
Orbital period
508.52 mins
BSTAR
0.0020106
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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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359 mins | 2025-08-31 00:27:50.834Z | 163.273° S | 2025-08-31 05:45:50.834Z | 157.85° S | 39.339° | 2025-08-31 06:26:50.834Z | 94.17° ESE |
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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