TITAN 3C TRANSTAGE R/B, 7324
Orbit data source: Space-Track
TITAN 3C TRANSTAGE R/B, 7324 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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7324 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 TITAN 3C TRANSTAGE R/B
1 7324U 74039C 26071.77863052 -.00000189 00000-0 00000+0 0 9991
2 7324 2.9904 262.1612 0033833 80.8467 71.7698 1.00715742118651Epoch: 2026-03-12T18:41Z
TLE epoch observation values (Epoch: 2026-03-12T18:41:13.676Z)
Latitude
1.33822°
Longitude
-35.52672°
Altitude
35,617.71 km
Speed
3.083 km/s
True Right ascension
03h 40m 48s
True Declination
1° 20' 13"
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
04:19:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,805.904 km
Perigee altitude
35,521.424 km
Semi-major axis
42,041.801 km
Eccentricity
0.00338
Inclination
2.9904°
RAAN
262.1612°
Arg. of periapsis
80.8467°
True anomaly
72.13852°
Mean anomaly
71.7698°
Eccentric anomaly
71.95411°
Mean motion
0.25178 °/min
Orbital period
1,429.82 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 R/B 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 R/B is likely not visible in the next few days. |
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7324 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 descending 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 descending order |
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