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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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: 7 hours ago
TLE from 7 hours ago
0 HYSIS
1 43719U 18096A 26316.27390425 .00000984 00000-0 14123-3 0 9993
2 43719 97.9685 21.7210 0001474 74.3781 285.7592 14.78685113429309Epoch: 2026-11-12T06:34Z
TLE epoch observation values (Epoch: 2026-11-12T06:34:25.327Z)
Latitude
-0.00007°
Longitude
-128.29427°
Altitude
636.215 km
Speed
7.54 km/s
True Right ascension
01h 26m 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
09:32:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
631.556 km
Perigee altitude
629.49 km
Semi-major axis
7,008.66 km
Eccentricity
0.00015
Inclination
97.9685°
RAAN
21.721°
Arg. of periapsis
74.3781°
True anomaly
285.74294°
Mean anomaly
285.7592°
Eccentric anomaly
285.75107°
Mean motion
3.69905 °/min
Orbital period
97.32 mins
BSTAR
0.00014123
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-12 16:53:28.573Z | 30.835° NE | 2026-11-12 16:57:28.573Z | 109.614° ESE | 38.881° | 2026-11-12 17:00:28.573Z | 163.455° S |
| 4 mins | 2026-11-12 18:31:28.573Z | 322.753° NNW | 2026-11-12 18:33:28.573Z | 289.394° WNW | 18.431° | 2026-11-12 18:35:28.573Z | 258.552° W |
| 6 mins | 2026-11-13 03:50:28.573Z | 116.235° SE | 2026-11-13 03:52:28.573Z | 75.495° E | 30.57° | 2026-11-13 03:56:28.573Z | 8.941° NNE |
| 5 mins | 2026-11-13 05:27:28.573Z | 235.243° WSW | 2026-11-13 05:29:28.573Z | 273.993° WNW | 22.317° | 2026-11-13 05:32:28.573Z | 317.246° 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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