TITAN 3C TRANSTAGE DEB, 62724
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 62724 is space debris in GEO originally from a launch on Thu, 26 Sep 1968 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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62724 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 months ago
0 TITAN 3C TRANSTAGE DEB
1 62724U 68081AS 25058.34013748 -.00000136 00000-0 00000-0 0 9995
2 62724 4.6543 35.9399 1129064 297.9914 51.2321 0.98137048 7525
Epoch: 2025-02-27T08:09Z
TLE epoch observation values (Epoch: 2025-02-27T08:09:47.878Z)
Latitude
-0.00001°
Longitude
116.37169°
Altitude
33,726.701 km
Speed
3.25 km/s
True Right ascension
02h 24m 57s
True Declination
0° 00' 00"
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
13:34:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
41,226.505 km
Perigee altitude
31,567.348 km
Semi-major axis
42,775.064 km
Eccentricity
0.11291
Inclination
4.6543°
RAAN
35.9399°
Arg. of periapsis
297.9914°
True anomaly
62.22495°
Mean anomaly
51.2321°
Eccentric anomaly
56.63495°
Mean motion
0.24533 °/min
Orbital period
1,467.39 mins
BSTAR
0
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Other satellites on launch #81 in the year 1968 (1968-09-26 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. |
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62724 neighbors
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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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