SCATSAT 1, 41790
Orbit data source: Space-Track
SCATSAT 1, 41790 is a payload satellite owned by ISRO (IN) in SSO that was launched on Mon, 26 Sep 2016 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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41790 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO SAC/Banga
Mission
Operational Civil Science
Bus & Motor
SSB-2, Unknown motor
Mass
370 kg wet, ~350 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: 15 hours ago
TLE from 15 hours ago
0 SCATSAT 1
1 41790U 16059H 25258.14768671 .00001669 00000-0 23015-3 0 9990
2 41790 98.1599 313.6713 0056735 54.6393 306.0101 14.78491530 60935Epoch: 2025-09-15T03:32Z
TLE epoch observation values (Epoch: 2025-09-15T03:32:40.131Z)
Latitude
-0.00001°
Longitude
-93.85242°
Altitude
613.855 km
Speed
7.565 km/s
True Right ascension
20h 54m 41s
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
11:10:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
670.911 km
Perigee altitude
591.377 km
Semi-major axis
7,009.281 km
Eccentricity
0.00567
Inclination
98.1599°
RAAN
313.6713°
Arg. of periapsis
54.6393°
True anomaly
305.482°
Mean anomaly
306.0101°
Eccentric anomaly
305.74627°
Mean motion
3.69856 °/min
Orbital period
97.34 mins
BSTAR
0.00023015
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Other satellites on launch #59 in the year 2016 (2016-09-26 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.SCATSAT 1 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-16 04:02:28.530Z | 183.881° SSW | 2025-09-16 04:05:28.530Z | 283.708° WNW | 40.101° | 2025-09-16 04:08:28.530Z | 337.063° NNW |
| 5 mins | 2025-09-16 15:52:28.530Z | 56.3° ENE | 2025-09-16 15:54:28.530Z | 93.641° ESE | 22.438° | 2025-09-16 15:57:28.530Z | 144.581° SSE |
| 6 mins | 2025-09-16 17:28:28.530Z | 337.791° N | 2025-09-16 17:30:28.530Z | 301.063° NW | 25.058° | 2025-09-16 17:34:28.530Z | 232.952° WSW |
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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