SS3 R/B, 60457
Orbit data source: Space-Track
SS3 R/B, 60457 is space debris in LEO originally from a launch on Fri, 16 Aug 2024 UTC launched from the Sirharikota (SRI). 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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60457 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 SS3 R/B
1 60457U 24147D   25308.29603885  .00308603  39433-4  81996-3 0  9991
2 60457  37.3539 321.7166 0010573 215.9675 144.0393 15.93528642 69397Epoch: 2025-11-04T07:06Z
TLE epoch observation values (Epoch: 2025-11-04T07:06:17.756Z)
Latitude
-0.00004°
Longitude
171.35746°
Altitude
297.258 km
Speed
7.728 km/s
True Right ascension
21h 26m 51s
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
07:13:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
302.435 km
Perigee altitude
288.323 km
Semi-major axis
6,673.516 km
Eccentricity
0.00106
Inclination
37.3539°
RAAN
321.7166°
Arg. of periapsis
215.9675°
True anomaly
144.11037°
Mean anomaly
144.0393°
Eccentric anomaly
144.07484°
Mean motion
3.98117 °/min
Orbital period
90.43 mins
BSTAR
0.00081996
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Other satellites on launch #147 in the year 2024 (2024-08-16 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.SS3 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.  | 
|---|---|---|---|---|---|---|---|
| SS3 R/B is likely not visible in the next few days. | 
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 ascending 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 ascending order  | 
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