TITAN 4 CENTAUR R/B, 23247
Orbit data source: Space-Track
TITAN 4 CENTAUR R/B, 23247 is space debris in GEO originally from a launch on Sat, 27 Aug 1994 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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23247 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 TITAN 4 CENTAUR R/B
1 23247U 94054B 26167.00264295 -.00000200 00000-0 00000-0 0 9993
2 23247 12.2390 354.4444 0114772 354.8384 5.0330 0.99579945 25513Epoch: 2026-06-16T00:03Z
TLE epoch observation values (Epoch: 2026-06-16T00:03:48.350Z)
Latitude
0.00002°
Longitude
89.20284°
Altitude
35,499.759 km
Speed
3.103 km/s
True Right ascension
23h 37m 44s
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
11:55:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,468.844 km
Perigee altitude
35,496.477 km
Semi-major axis
42,360.798 km
Eccentricity
0.01148
Inclination
12.239°
RAAN
354.4444°
Arg. of periapsis
354.8384°
True anomaly
5.15005°
Mean anomaly
5.033°
Eccentric anomaly
5.09136°
Mean motion
0.24894 °/min
Orbital period
1,446.12 mins
BSTAR
0
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Other satellites on launch #54 in the year 1994 (1994-08-27 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 4 CENTAUR 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 4 CENTAUR R/B is likely not visible in the next few days. |
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23247 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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