PRATHAM, 41783
Orbit data source: Space-Track
PRATHAM, 41783 is a payload satellite owned by IITB (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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41783 intel report (Beta)
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Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
IITB
Mission
Non-operational Amateur Science
Bus & Motor
PRATHAM, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.189 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 PRATHAM
1 41783U 16059A 26277.22009417 .00000334 00000-0 67115-4 0 9997
2 41783 97.8421 269.3466 0030004 229.8222 130.0356 14.67312162535505Epoch: 2026-10-04T05:16Z
TLE epoch observation values (Epoch: 2026-10-04T05:16:56.136Z)
Latitude
0.00002°
Longitude
177.19623°
Altitude
686.31 km
Speed
7.506 km/s
True Right ascension
17h 57m 23s
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
22:23:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
687.854 km
Perigee altitude
645.58 km
Semi-major axis
7,044.854 km
Eccentricity
0.003
Inclination
97.8421°
RAAN
269.3466°
Arg. of periapsis
229.8222°
True anomaly
130.29821°
Mean anomaly
130.0356°
Eccentric anomaly
130.16697°
Mean motion
3.67058 °/min
Orbital period
98.08 mins
BSTAR
0.000067115
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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.PRATHAM 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 | 2026-10-05 11:20:19.699Z | 52.421° ENE | 2026-10-05 11:23:19.699Z | 93.887° ESE | 16.747° | 2026-10-05 11:25:19.699Z | 123.232° SE |
| 7 mins | 2026-10-05 12:57:19.699Z | 353.601° N | 2026-10-05 13:00:19.699Z | 296.33° NW | 44.429° | 2026-10-05 13:04:19.699Z | 218.403° SW |
| 8 mins | 2026-10-05 23:57:19.699Z | 186.552° SSW | 2026-10-06 00:01:19.699Z | 282.694° WNW | 51.494° | 2026-10-06 00:05:19.699Z | 337.47° 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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