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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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: 13 hours ago
TLE from 13 hours ago
0 SDX02
1 62460U 24253B 25318.90272791 .00048080 00000-0 91837-3 0 9991
2 62460 54.9968 260.2727 0008198 49.0852 311.0889 15.47672535 49133Epoch: 2025-11-14T21:39Z
TLE epoch observation values (Epoch: 2025-11-14T21:39:55.691Z)
Latitude
-0°
Longitude
-118.9489°
Altitude
420.978 km
Speed
7.662 km/s
True Right ascension
17h 21m 05s
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
07:31:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
429.075 km
Perigee altitude
417.923 km
Semi-major axis
6,801.636 km
Eccentricity
0.00082
Inclination
54.9968°
RAAN
260.2727°
Arg. of periapsis
49.0852°
True anomaly
311.01805°
Mean anomaly
311.0889°
Eccentric anomaly
311.05348°
Mean motion
3.86922 °/min
Orbital period
93.04 mins
BSTAR
0.00091837
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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 | 2025-11-15 22:38:26.633Z | 222.751° SW | 2025-11-15 22:41:26.633Z | 61.697° ENE | 42.14° | 2025-11-15 22:43:26.633Z | 49.014° ENE |
| 5 mins | 2025-11-16 05:09:26.633Z | 339.473° N | 2025-11-16 05:11:26.633Z | 37.406° NE | 29.513° | 2025-11-16 05:14:26.633Z | 103.894° ESE |
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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