DSAT, 42794
Orbit data source: Space-Track
DSAT, 42794 is a payload satellite owned by D-ORBIT (IT) in SSO that was launched on Fri, 23 Jun 2017 UTC via a PSLV-XL 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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42794 intel report (Beta)
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Identifier
Orbit
Country
ITRelated business
Manufacturer
D-ORBIT
Mission
Non-operational Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4.5 kg wet, 4.2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 DSAT
1 42794U 17036AF 26062.18188499 .00007797 00000-0 38052-3 0 9998
2 42794 97.5470 41.5602 0084694 167.5584 192.7767 15.15394512474791Epoch: 2026-03-03T04:21Z
TLE epoch observation values (Epoch: 2026-03-03T04:21:54.863Z)
Latitude
0.00001°
Longitude
175.11698°
Altitude
579.873 km
Speed
7.539 km/s
True Right ascension
02h 46m 14s
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
15:17:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.154 km
Perigee altitude
458.363 km
Semi-major axis
6,894.896 km
Eccentricity
0.00847
Inclination
97.547°
RAAN
41.5602°
Arg. of periapsis
167.5584°
True anomaly
192.56426°
Mean anomaly
192.7767°
Eccentric anomaly
192.67026°
Mean motion
3.79098 °/min
Orbital period
94.96 mins
BSTAR
0.00038052
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Other satellites on launch #36 in the year 2017 (2017-06-23 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.DSAT 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 | 2026-03-03 21:55:47.727Z | 131.772° SE | 2026-03-03 21:58:47.727Z | 81.916° E | 26.18° | 2026-03-03 22:01:47.727Z | 16.65° NNE |
| 4 mins | 2026-03-03 23:31:47.727Z | 237.806° WSW | 2026-03-03 23:32:47.727Z | 255.998° W | 17.522° | 2026-03-03 23:35:47.727Z | 308.36° NW |
| 5 mins | 2026-03-04 11:03:47.727Z | 39.8° NE | 2026-03-04 11:05:47.727Z | 107.385° ESE | 33.114° | 2026-03-04 11:08:47.727Z | 170.462° S |
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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