SDX01, 62459 (Decayed)
Orbit data source: Space-Track
SDX01, 62459 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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62459 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: 3 weeks ago
TLE from 3 weeks ago
0 SDX01
1 62459U 24253A 26285.57467329 .12462361 12221-4 34974-3 0 9995
2 62459 54.9797 141.8233 0006916 269.5316 90.4966 16.45004478101145Epoch: 2026-10-12T13:47Z
TLE epoch observation values (Epoch: 2026-10-12T13:47:31.772Z)
Latitude
-0.00003°
Longitude
-86.21024°
Altitude
153.713 km
Speed
7.815 km/s
True Right ascension
09h 27m 17s
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
10:45:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
157.004 km
Perigee altitude
147.971 km
Semi-major axis
6,530.624 km
Eccentricity
0.00069
Inclination
54.9797°
RAAN
141.8233°
Arg. of periapsis
269.5316°
True anomaly
90.57585°
Mean anomaly
90.4966°
Eccentric anomaly
90.53622°
Mean motion
4.11255 °/min
Orbital period
87.54 mins
BSTAR
0.00034974
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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.SDX01 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
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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