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: 11 hours ago
TLE from 11 hours ago
0 DSAT
1 42794U 17036AF 26095.45496390 .00012279 00000-0 58482-3 0 9996
2 42794 97.5523 74.6383 0084946 54.6629 306.2507 15.16067197479830Epoch: 2026-04-05T10:55Z
TLE epoch observation values (Epoch: 2026-04-05T10:55:08.880Z)
Latitude
-0°
Longitude
77.09116°
Altitude
486.502 km
Speed
7.641 km/s
True Right ascension
04h 58m 33s
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
03:23:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.27 km
Perigee altitude
456.166 km
Semi-major axis
6,892.855 km
Eccentricity
0.00849
Inclination
97.5523°
RAAN
74.6383°
Arg. of periapsis
54.6629°
True anomaly
305.46077°
Mean anomaly
306.2507°
Eccentric anomaly
305.85623°
Mean motion
3.79267 °/min
Orbital period
94.92 mins
BSTAR
0.00058482
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-05 22:08:25.855Z | 137.894° SSE | 2026-04-05 22:11:25.855Z | 65.489° ENE | 29.895° | 2026-04-05 22:13:25.855Z | 14.279° NNE |
| 6 mins | 2026-04-06 11:14:25.855Z | 22.082° NNE | 2026-04-06 11:17:25.855Z | 114.912° SE | 41.118° | 2026-04-06 11:20:25.855Z | 180.539° SSW |
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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