SS3 R/B, 60457 (Decayed)
Orbit data source: Space-Track
SS3 R/B, 60457 was 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
Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Decayed spacecraft
Bus & Motor
SS-3, Unknown motor
Mass
~400 kg wet, ~400 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.4 m
Radar Cross Section
5.969 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 weeks ago
TLE from 4 weeks ago
0 SS3 R/B
1 60457U 24147D 25330.29463554 .06855926 41750-5 56446-3 0 9992
2 60457 37.3387 169.6446 0004584 295.7733 64.2588 16.38654489 72936Epoch: 2025-11-26T07:04Z
TLE epoch observation values (Epoch: 2025-11-26T07:04:16.510Z)
Latitude
0.00002°
Longitude
-1.89213°
Altitude
167.195 km
Speed
7.809 km/s
True Right ascension
11h 18m 34s
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
22:15:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
175.407 km
Perigee altitude
169.401 km
Semi-major axis
6,550.541 km
Eccentricity
0.00046
Inclination
37.3387°
RAAN
169.6446°
Arg. of periapsis
295.7733°
True anomaly
64.30613°
Mean anomaly
64.2588°
Eccentric anomaly
64.28246°
Mean motion
4.09381 °/min
Orbital period
87.94 mins
BSTAR
0.00056446
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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. |
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| This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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