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: 9 hours ago
TLE from 9 hours ago
0 DSAT
1 42794U 17036AF 26093.87090410 .00016946 00000-0 80598-3 0 9991
2 42794 97.5519 73.0618 0085109 59.9962 300.9682 15.16025401479599Epoch: 2026-04-03T20:54Z
TLE epoch observation values (Epoch: 2026-04-03T20:54:06.114Z)
Latitude
-0.00001°
Longitude
-72.66249°
Altitude
491.111 km
Speed
7.636 km/s
True Right ascension
04h 52m 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
11:27:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.51 km
Perigee altitude
456.179 km
Semi-major axis
6,892.981 km
Eccentricity
0.00851
Inclination
97.5519°
RAAN
73.0618°
Arg. of periapsis
59.9962°
True anomaly
300.12737°
Mean anomaly
300.9682°
Eccentric anomaly
300.54824°
Mean motion
3.79256 °/min
Orbital period
94.92 mins
BSTAR
0.00080598
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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 | 2026-04-04 11:42:39.174Z | 0.15° NNE | 2026-04-04 11:45:39.174Z | 286.555° WNW | 38.801° | 2026-04-04 11:48:39.174Z | 210.564° SW |
| 5 mins | 2026-04-04 22:23:39.174Z | 145.432° SSE | 2026-04-04 22:25:39.174Z | 56.091° ENE | 39.495° | 2026-04-04 22:28:39.174Z | 356.799° N |
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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