PISAT, 41784
Orbit data source: Space-Track
PISAT, 41784 is a payload satellite owned by PES Univ. (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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41784 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
PES Univ.
Mission
Operational Amateur Imaging
Bus & Motor
PISAT, Unknown motor
Mass
5.25 kg wet, 5.25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.063 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 PISAT
1 41784U 16059B 26092.73671791 .00001452 00000-0 25494-3 0 9994
2 41784 97.8191 96.4381 0030594 86.8133 273.6572 14.68836341508663Epoch: 2026-04-02T17:40Z
TLE epoch observation values (Epoch: 2026-04-02T17:40:52.427Z)
Latitude
-0.00009°
Longitude
0.13875°
Altitude
666.485 km
Speed
7.525 km/s
True Right ascension
06h 25m 45s
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
09:32:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
683.376 km
Perigee altitude
640.299 km
Semi-major axis
7,039.975 km
Eccentricity
0.00306
Inclination
97.8191°
RAAN
96.4381°
Arg. of periapsis
86.8133°
True anomaly
273.30725°
Mean anomaly
273.6572°
Eccentric anomaly
273.48223°
Mean motion
3.6744 °/min
Orbital period
97.98 mins
BSTAR
0.00025494
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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.PISAT 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-03 12:14:53.379Z | 42.165° NE | 2026-04-03 12:17:53.379Z | 88.56° E | 23.186° | 2026-04-03 12:21:53.379Z | 151.592° SSE |
| 6 mins | 2026-04-03 13:52:53.379Z | 334.82° NNW | 2026-04-03 13:54:53.379Z | 297.214° NW | 25.063° | 2026-04-03 13:58:53.379Z | 232.759° WSW |
| 4 mins | 2026-04-03 23:16:53.379Z | 96.392° ESE | 2026-04-03 23:18:53.379Z | 58.495° ENE | 20.527° | 2026-04-03 23:20:53.379Z | 26.511° NE |
| 6 mins | 2026-04-04 00:52:53.379Z | 213.183° SW | 2026-04-04 00:54:53.379Z | 252.516° W | 27.827° | 2026-04-04 00:58:53.379Z | 324.771° NNW |
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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