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: 10 hours ago
TLE from 10 hours ago
0 HYSIS
1 43719U 18096A 25306.51479034 .00001690 00000-0 23776-3 0 9991
2 43719 98.0149 9.6788 0001577 118.1085 242.0286 14.78666619373921Epoch: 2025-11-02T12:21Z
TLE epoch observation values (Epoch: 2025-11-02T12:21:17.885Z)
Latitude
0.00004°
Longitude
142.32485°
Altitude
637.071 km
Speed
7.539 km/s
True Right ascension
00h 38m 42s
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
18:36:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
631.689 km
Perigee altitude
629.479 km
Semi-major axis
7,008.721 km
Eccentricity
0.00016
Inclination
98.0149°
RAAN
9.6788°
Arg. of periapsis
118.1085°
True anomaly
242.01264°
Mean anomaly
242.0286°
Eccentric anomaly
242.02062°
Mean motion
3.69901 °/min
Orbital period
97.32 mins
BSTAR
0.00023776
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-03 03:08:25.728Z | 94.085° ESE | 2025-11-03 03:10:25.728Z | 65.029° ENE | 14.52° | 2025-11-03 03:12:25.728Z | 35.704° NE |
| 7 mins | 2025-11-03 04:43:25.728Z | 190.353° SSW | 2025-11-03 04:46:25.728Z | 261.342° W | 37.419° | 2025-11-03 04:50:25.728Z | 335.423° NNW |
| 6 mins | 2025-11-03 16:33:25.728Z | 46.247° ENE | 2025-11-03 16:36:25.728Z | 108.604° ESE | 26.108° | 2025-11-03 16:39:25.728Z | 155.719° SSE |
| 5 mins | 2025-11-03 18:10:25.728Z | 325.546° NNW | 2025-11-03 18:12:25.728Z | 286.962° WNW | 21.518° | 2025-11-03 18:15:25.728Z | 241.514° WSW |
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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