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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Edit Public Description
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: 17 hours ago
TLE from 17 hours ago
0 DSAT
1 42794U 17036AF 25356.49544357 .00010541 00000-0 53274-3 0 9990
2 42794 97.5376 331.4740 0088747 53.9861 306.9555 15.13795807464095Epoch: 2025-12-22T11:53Z
TLE epoch observation values (Epoch: 2025-12-22T11:53:26.324Z)
Latitude
-0.00003°
Longitude
61.8216°
Altitude
491.228 km
Speed
7.639 km/s
True Right ascension
22h 05m 53s
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
04:24:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.849 km
Perigee altitude
460.383 km
Semi-major axis
6,899.753 km
Eccentricity
0.00887
Inclination
97.5376°
RAAN
331.474°
Arg. of periapsis
53.9861°
True anomaly
306.13741°
Mean anomaly
306.9555°
Eccentric anomaly
306.547°
Mean motion
3.78698 °/min
Orbital period
95.06 mins
BSTAR
0.00053274
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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 | 2025-12-23 10:40:21.258Z | 47.033° ENE | 2025-12-23 10:42:21.258Z | 84.375° E | 21.864° | 2025-12-23 10:45:21.258Z | 145.872° SSE |
| 4 mins | 2025-12-23 12:15:21.258Z | 323.033° NNW | 2025-12-23 12:17:21.258Z | 279.982° WNW | 19.311° | 2025-12-23 12:19:21.258Z | 245.481° WSW |
| 4 mins | 2025-12-23 22:56:21.258Z | 208.156° SW | 2025-12-23 22:57:21.258Z | 240.732° WSW | 32.796° | 2025-12-23 23:00:21.258Z | 329.133° 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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