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: 12 hours ago
TLE from 12 hours ago
0 HYSIS
1 43719U 18096A 25357.33563567 .00001368 00000-0 19372-3 0 9991
2 43719 98.0084 60.2613 0000908 54.4466 305.6829 14.78671914381439Epoch: 2025-12-23T08:03Z
TLE epoch observation values (Epoch: 2025-12-23T08:03:18.921Z)
Latitude
-0.00009°
Longitude
-152.68838°
Altitude
636.164 km
Speed
7.54 km/s
True Right ascension
04h 01m 02s
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
19:01:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
631.203 km
Perigee altitude
629.931 km
Semi-major axis
7,008.704 km
Eccentricity
0.00009
Inclination
98.0084°
RAAN
60.2613°
Arg. of periapsis
54.4466°
True anomaly
305.67445°
Mean anomaly
305.6829°
Eccentric anomaly
305.67867°
Mean motion
3.69902 °/min
Orbital period
97.32 mins
BSTAR
0.00019372
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-24 03:41:08.984Z | 125.226° SE | 2025-12-24 03:44:08.984Z | 70.251° E | 27.138° | 2025-12-24 03:47:08.984Z | 14.802° NNE |
| 5 mins | 2025-12-24 05:18:08.984Z | 224.046° SW | 2025-12-24 05:20:08.984Z | 257.302° W | 20.585° | 2025-12-24 05:23:08.984Z | 309.096° NW |
| 7 mins | 2025-12-24 17:07:08.984Z | 21.083° NNE | 2025-12-24 17:10:08.984Z | 112.546° SE | 43.124° | 2025-12-24 17:14:08.984Z | 185.459° SSW |
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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