SDX02, 62460
Orbit data source: Space-Track
SDX02, 62460 is 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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SDX02 radio frequencies
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Edit Public Description
Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Operational 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: 6 hours ago
TLE from 6 hours ago
0 SDX02
1 62460U 24253B 25258.99736108 .00031585 00000-0 71549-3 0 9990
2 62460 54.9966 172.5459 0005143 180.7269 179.3754 15.42879481 39870Epoch: 2025-09-15T23:56Z
TLE epoch observation values (Epoch: 2025-09-15T23:56:11.997Z)
Latitude
-0.00004°
Longitude
178.30189°
Altitude
442.222 km
Speed
7.646 km/s
True Right ascension
11h 30m 11s
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
22:17:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
441.084 km
Perigee altitude
434.073 km
Semi-major axis
6,815.716 km
Eccentricity
0.00051
Inclination
54.9966°
RAAN
172.5459°
Arg. of periapsis
180.7269°
True anomaly
179.37604°
Mean anomaly
179.3754°
Eccentric anomaly
179.37572°
Mean motion
3.85723 °/min
Orbital period
93.33 mins
BSTAR
0.00071549
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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 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-16 20:18:43.955Z | 194.668° SSW | 2025-09-16 20:20:43.955Z | 149.948° SSE | 30.96° | 2025-09-16 20:23:43.955Z | 65.818° ENE |
| 4 mins | 2025-09-16 21:56:43.955Z | 292.558° NW | 2025-09-16 21:57:43.955Z | 316.45° NNW | 21.319° | 2025-09-16 22:00:43.955Z | 21.121° NNE |
| 5 mins | 2025-09-17 04:27:43.955Z | 289.747° WNW | 2025-09-17 04:29:43.955Z | 223.807° SW | 33.899° | 2025-09-17 04:32:43.955Z | 157.142° SSE |
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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