TITAN 3C TRANSTAGE DEB, 26526
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 26526 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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26526 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 9 months ago
0 TITAN 3C TRANSTAGE DEB
1 26526U 65108AM 24298.24131281 .00000584 00000-0 35549-2 0 9993
2 26526 27.0953 271.9805 6511654 243.4914 289.0941 3.11000988 61163
Epoch: 2024-10-24T05:47Z
TLE epoch observation values (Epoch: 2024-10-24T05:47:29.426Z)
Latitude
26.55104°
Longitude
-105.36752°
Altitude
17,158.249 km
Speed
3.711 km/s
True Right ascension
00h 58m 31s
True Declination
26° 30' 34"
Sunlit
Visualization orbit readout
Latitude
-22.16772°
Longitude
-39.48211°
Altitude
24,923.516 km
Speed
2.313 km/s
Apparent Right ascension
05h 59m 02s
Apparent Declination
-30° 21' 23"
Sunlit
Visualization observer readout
Local Sidereal Time
01:11:30
Azimuth
124.317° SE
Elevation
-6.804°
Doppler factor
1
Orbital elements
Apogee altitude
26,363.083 km
Perigee altitude
538.959 km
Semi-major axis
19,829.158 km
Eccentricity
0.65117
Inclination
27.0953°
RAAN
271.9805°
Arg. of periapsis
243.4914°
True anomaly
217.79082°
Mean anomaly
289.0941°
Eccentric anomaly
253.34944°
Mean motion
0.7773 °/min
Orbital period
463.14 mins
BSTAR
0.0035549
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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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48 mins | 2025-07-19 22:01:46.599Z | 229.184° WSW | 2025-07-19 22:42:46.599Z | 178.946° S | 28.008° | 2025-07-19 22:49:46.599Z | 124.4° SE |
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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