HYSIS, 43719
Orbit data source: Space-Track
HYSIS, 43719 is a payload satellite owned by ISRO (IN) in SSO that was launched on Thu, 29 Nov 2018 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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43719 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
ISRO
Mission
Operational Civil Imaging
Bus & Motor
SSB-2, AOCS
Mass
380 kg wet, ~350 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
4.485 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 HYSIS
1 43719U 18096A 25261.31034325 .00001107 00000-0 15822-3 0 9995
2 43719 98.0213 324.6515 0000524 116.5874 243.5391 14.78664662367247Epoch: 2025-09-18T07:26Z
TLE epoch observation values (Epoch: 2025-09-18T07:26:53.656Z)
Latitude
-0°
Longitude
-144.54584°
Altitude
636.722 km
Speed
7.54 km/s
True Right ascension
21h 38m 36s
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
06:42:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.958 km
Perigee altitude
630.223 km
Semi-major axis
7,008.727 km
Eccentricity
0.00005
Inclination
98.0213°
RAAN
324.6515°
Arg. of periapsis
116.5874°
True anomaly
243.53372°
Mean anomaly
243.5391°
Eccentric anomaly
243.53641°
Mean motion
3.699 °/min
Orbital period
97.32 mins
BSTAR
0.00015822
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Other satellites on launch #96 in the year 2018 (2018-11-29 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.HYSIS 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 | 2025-09-18 16:09:33.223Z | 51.988° ENE | 2025-09-18 16:12:33.223Z | 96.853° ESE | 16.969° | 2025-09-18 16:14:33.223Z | 127.799° SE |
| 6 mins | 2025-09-18 17:46:33.223Z | 343.162° N | 2025-09-18 17:48:33.223Z | 298.844° NW | 31.668° | 2025-09-18 17:52:33.223Z | 222.411° SW |
| 7 mins | 2025-09-19 04:41:33.223Z | 191.526° SSW | 2025-09-19 04:44:33.223Z | 271.059° WNW | 37.297° | 2025-09-19 04:48:33.223Z | 336.242° 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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