HYSIS
NORAD 43719
Payload
LEO
2018-096A
● Active
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LEO · NORAD 43719
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
632 km
Apogee
635 km
Inclination
98.0°
Period
97.4 min
Mean Motion
14.78619131 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude634 km
Orbital Velocity27,157 km/h
Velocity7.54 km/s
Orbital Period97 minutes
Orbits / Day14.79
Eccentricity0.0002
Semi-Major Axis7,005 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇮🇳 Indian Space Research Organization (ISRO) (India)
Launch Date
2018-11-29
Launch Site
SRI
Int'l Designator
2018-096A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
HYSIS is an active satellite operated by Indian Space Research Organization (ISRO) (India), launched on 2018-11-29 from SRI. It orbits in Low Earth Orbit (LEO) at altitudes between 632 km and 635 km with an inclination of 98.0°. It travels at approximately 27,157 km/h (7.54 km/s), completing one full orbit every 97 minutes — that’s roughly 14.79 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks HYSIS in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
HYSIS orbits at an average altitude of 634 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of HYSIS’s average altitude, there are currently 776 active payloads and 876 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050. With an inclination of 98.0°, HYSIS passes over latitudes between 98.0°N and 98.0°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. India operates approximately 108 active satellites in total, of which 12 share a similar altitude band with HYSIS.
❓ Frequently Asked Questions
HYSIS is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 634 km altitude. Its 98.0° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 97 minutes, travelling at 27,157 km/h.
HYSIS is operated by Indian Space Research Organization (ISRO) (India). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43719. You can track HYSIS in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
HYSIS was launched on 2018-11-29 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks HYSIS (NORAD ID 43719) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
HYSIS travels at approximately 27,157 km/h (16,875 mph) — roughly 7.54 km/s. It completes 14.79 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.