TITAN 3C TRANSTAGE DEB, 26527
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 26527 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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26527 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 TITAN 3C TRANSTAGE DEB
1 26527U 65108AN 25080.34198972 .00000167 00000-0 48222-2 0 9994
2 26527 26.7272 132.7655 6755729 217.5552 156.4621 2.71379379257509
Epoch: 2025-03-21T08:12Z
TLE epoch observation values (Epoch: 2025-03-21T08:12:27.911Z)
Latitude
13.52634°
Longitude
-140.92447°
Altitude
29,561.204 km
Speed
1.956 km/s
True Right ascension
10h 45m 10s
True Declination
13° 30' 39"
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
16:05:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
30,006.502 km
Perigee altitude
666.715 km
Semi-major axis
21,714.745 km
Eccentricity
0.67557
Inclination
26.7272°
RAAN
132.7655°
Arg. of periapsis
217.5552°
True anomaly
173.7681°
Mean anomaly
156.4621°
Eccentric anomaly
165.89506°
Mean motion
0.67828 °/min
Orbital period
530.75 mins
BSTAR
0.0048222
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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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350 mins | 2025-08-31 18:37:50.005Z | 254.476° W | 2025-08-31 19:23:50.005Z | 179.557° S | 43.278° | 2025-09-01 00:27:50.005Z | 187.632° SSW |
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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