SDX02, 62460 (Decayed)
Orbit data source: Space-Track
SDX02, 62460 was a payload satellite owned by ISRO (IN) in LEO that was launched on Mon, 30 Dec 2024 UTC via a PSLV launch vehicle from the Sirharikota (SRI). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62460 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Decayed Civil Technology
Bus & Motor
SPADEX, Unknown motor
Mass
220 kg wet, ~180 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.3 m
Radar Cross Section
0.901 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 SDX02
1 62460U 24253B 26285.83165238 .11551553 12210-4 46502-3 0 9999
2 62460 54.9815 140.6438 0006314 286.0781 73.9598 16.43456969101178Epoch: 2026-10-12T19:57Z
TLE epoch observation values (Epoch: 2026-10-12T19:57:34.765Z)
Latitude
-0°
Longitude
179.84452°
Altitude
156.632 km
Speed
7.814 km/s
True Right ascension
09h 22m 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
09:37:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
160.712 km
Perigee altitude
152.46 km
Semi-major axis
6,534.723 km
Eccentricity
0.00063
Inclination
54.9815°
RAAN
140.6438°
Arg. of periapsis
286.0781°
True anomaly
74.02935°
Mean anomaly
73.9598°
Eccentric anomaly
73.99457°
Mean motion
4.10868 °/min
Orbital period
87.62 mins
BSTAR
0.00046502
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Other satellites on launch #253 in the year 2024 (2024-12-30 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.SDX02 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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