SL-16 R/B, 24298
Orbit data source: Space-Track
SL-16 R/B, 24298 is space debris in LEO originally from a launch on Wed, 04 Sep 1996 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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24298 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 SL-16 R/B
1 24298U 96051B 26138.92439152 .00000121 00000-0 91996-4 0 9993
2 24298 70.7634 26.5822 0013240 24.1420 336.0318 14.12435260531564Epoch: 2026-05-18T22:11Z
TLE epoch observation values (Epoch: 2026-05-18T22:11:07.427Z)
Latitude
0.00004°
Longitude
177.1956°
Altitude
844.687 km
Speed
7.435 km/s
True Right ascension
01h 46m 19s
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
14:41:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
858.57 km
Perigee altitude
839.432 km
Semi-major axis
7,227.138 km
Eccentricity
0.00132
Inclination
70.7634°
RAAN
26.5822°
Arg. of periapsis
24.142°
True anomaly
335.97007°
Mean anomaly
336.0318°
Eccentric anomaly
336.00095°
Mean motion
3.53259 °/min
Orbital period
101.91 mins
BSTAR
0.000091996
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Other satellites on launch #51 in the year 1996 (1996-09-04 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.SL-16 R/B 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-05-19 16:59:39.073Z | 161.767° S | 2026-05-19 17:03:39.073Z | 112.21° ESE | 27.172° | 2026-05-19 17:08:39.073Z | 45.146° ENE |
| 8 mins | 2026-05-19 18:44:39.073Z | 244.826° WSW | 2026-05-19 18:48:39.073Z | 311.538° NW | 29.965° | 2026-05-19 18:52:39.073Z | 3.708° NNE |
| 5 mins | 2026-05-20 01:56:39.073Z | 24.502° NE | 2026-05-20 01:58:39.073Z | 48.36° ENE | 15.801° | 2026-05-20 02:01:39.073Z | 82.669° E |
| 9 mins | 2026-05-20 03:39:39.073Z | 333.388° NNW | 2026-05-20 03:43:39.073Z | 258.768° W | 44.612° | 2026-05-20 03:48:39.073Z | 162.81° S |
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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