TITAN 3C TRANSTAGE DEB, 43456
Orbit data source: Space-Track
TITAN 3C TRANSTAGE DEB, 43456 is space debris in GEO originally from a launch on Sun, 09 Feb 1969 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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Martin Marietta
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 TITAN 3C TRANSTAGE DEB
1 43456U 69013P 25339.09661363 -.00000165 00000-0 00000+0 0 9999
2 43456 1.5793 45.4615 0518571 90.7208 274.3659 1.02726773 29076Epoch: 2025-12-05T02:19Z
TLE epoch observation values (Epoch: 2025-12-05T02:19:07.417Z)
Latitude
0.00139°
Longitude
-64.31555°
Altitude
35,051.069 km
Speed
3.104 km/s
True Right ascension
02h 58m 26s
True Declination
0° 00' 05"
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
09:57:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
37,264.826 km
Perigee altitude
32,961.585 km
Semi-major axis
41,491.343 km
Eccentricity
0.05186
Inclination
1.5793°
RAAN
45.4615°
Arg. of periapsis
90.7208°
True anomaly
268.42207°
Mean anomaly
274.3659°
Eccentric anomaly
271.39559°
Mean motion
0.25681 °/min
Orbital period
1,401.83 mins
BSTAR
0
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Other satellites on launch #13 in the year 1969 (1969-02-09 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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 20 mins | 2025-12-06 11:56:14.675Z | 106.512° ESE | 2025-12-06 11:56:14.675Z | 106.512° ESE | 10.226° | 2025-12-06 12:16:14.675Z | 106.463° ESE |
| 852 mins | 2025-12-06 16:20:14.675Z | 108.146° ESE | 2025-12-07 00:47:14.675Z | 111.976° ESE | 14.927° | 2025-12-07 06:32:14.675Z | 104.77° ESE |
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43456 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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