TITAN 3C TRANSTAGE DEB, 53647
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 53647 is space debris in GEO originally from a launch on Thu, 30 May 1974 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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53647 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 TITAN 3C TRANSTAGE DEB
1 53647U 74039D 24273.63213551 .00000067 00000-0 00000-0 0 9995
2 53647 4.3498 272.7542 0236171 232.5063 124.8340 1.00609122 19
Epoch: 2024-09-29T15:10Z
TLE epoch observation values (Epoch: 2024-09-29T15:10:16.508Z)
Latitude
-0.01051°
Longitude
35.84639°
Altitude
36,272.027 km
Speed
3.036 km/s
True Right ascension
18h 09m 08s
True Declination
0° 00' 38"
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
09:36:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,686.963 km
Perigee altitude
34,699.749 km
Semi-major axis
42,071.493 km
Eccentricity
0.02362
Inclination
4.3498°
RAAN
272.7542°
Arg. of periapsis
232.5063°
True anomaly
127.01799°
Mean anomaly
124.834°
Eccentric anomaly
125.9297°
Mean motion
0.25151 °/min
Orbital period
1,431.33 mins
BSTAR
0
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Other satellites on launch #39 in the year 1974 (1974-05-30 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
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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. |
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TITAN 3C TRANSTAGE DEB is likely not visible in the next few days. |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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