SL-23 R/B, 34112
Orbit data source: Space-Track
SL-23 R/B, 34112 is space debris in HEO originally from a launch on Thu, 26 Feb 2009 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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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34112 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 SL-23 R/B
1 34112U 09009B 25244.26786698 -.00000056 00000-0 00000-0 0 9990
2 34112 35.1814 341.4733 6894199 65.2928 349.8167 2.20444771132991
Epoch: 2025-09-01T06:25Z
TLE epoch observation values (Epoch: 2025-09-01T06:25:43.707Z)
Latitude
1.12295°
Longitude
-94.02892°
Altitude
3,628.749 km
Speed
7.98 km/s
True Right ascension
22h 52m 18s
True Declination
1° 07' 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
20:22:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,757.265 km
Perigee altitude
1,367.964 km
Semi-major axis
24,940.751 km
Eccentricity
0.68942
Inclination
35.1814°
RAAN
341.4733°
Arg. of periapsis
65.2928°
True anomaly
296.29104°
Mean anomaly
349.8167°
Eccentric anomaly
330.16468°
Mean motion
0.55103 °/min
Orbital period
653.32 mins
BSTAR
0
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Other satellites on launch #9 in the year 2009 (2009-02-26 UTC)
SL-23 R/B Visibility forecast
Observer location: undefined°, undefined°
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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25 mins | 2025-09-03 13:10:46.643Z | 262.721° W | 2025-09-03 13:17:46.643Z | 170.147° S | 42.946° | 2025-09-03 13:35:46.643Z | 101.091° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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