XPOSAT, 58694
Orbit data source: Space-Track
XPOSAT, 58694 is a payload satellite owned by ISRO (IN) in LEO that was launched on Mon, 01 Jan 2024 UTC via a PSLV-DL 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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58694 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Operational Civil Astronomy
Bus & Motor
IMS-2, Unknown motor
Mass
469 kg wet, 469 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.0 m
Radar Cross Section
4.015 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 XPOSAT
1 58694U 24001A 26076.76662780 .00001916 00000-0 16662-3 0 9993
2 58694 5.9863 122.0275 0009787 264.8772 95.0238 14.79082282119462Epoch: 2026-03-17T18:23Z
TLE epoch observation values (Epoch: 2026-03-17T18:23:56.641Z)
Latitude
-0.00001°
Longitude
30.70137°
Altitude
629.771 km
Speed
7.546 km/s
True Right ascension
08h 08m 06s
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
21:28:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
645.278 km
Perigee altitude
631.544 km
Semi-major axis
7,016.548 km
Eccentricity
0.00098
Inclination
5.9863°
RAAN
122.0275°
Arg. of periapsis
264.8772°
True anomaly
95.13551°
Mean anomaly
95.0238°
Eccentric anomaly
95.07966°
Mean motion
3.69282 °/min
Orbital period
97.49 mins
BSTAR
0.00016662
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Other satellites on launch #1 in the year 2024 (2024-01-01 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.XPOSAT 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. |
|---|---|---|---|---|---|---|---|
| XPOSAT is likely not visible in the next few days. |
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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