ZHANGHENG 1
NORAD 43194
Payload
LEO
2018-015C
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LEO · NORAD 43194
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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
491 km
Apogee
515 km
Inclination
97.7°
Period
94.7 min
Mean Motion
15.20921353 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude503 km
Orbital Velocity27,414 km/h
Velocity7.61 km/s
Orbital Period95 minutes
Orbits / Day15.21
Eccentricity0.0017
Semi-Major Axis6,874 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China Earthquake Administration/Italian Institute for Nuclear Physics (China)
Launch Date
2018-02-02
Launch Site
Jiuquan, China
Int'l Designator
2018-015C
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
ZHANGHENG 1 is an active satellite operated by China Earthquake Administration/Italian Institute for Nuclear Physics (China), launched on 2018-02-02 from Jiuquan, China on the CSES launch. It orbits in Low Earth Orbit (LEO) at altitudes between 491 km and 515 km with an inclination of 97.7°. It travels at approximately 27,414 km/h (7.61 km/s), completing one full orbit every 95 minutes — that’s roughly 15.21 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks ZHANGHENG 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ZHANGHENG 1 orbits at an average altitude of 503 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 ZHANGHENG 1’s average altitude, there are currently 9,647 active payloads and 244 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 55.2% of all active satellites. With an inclination of 97.7°, ZHANGHENG 1 passes over latitudes between 97.7°N and 97.7°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. China operates approximately 1,221 active satellites in total, of which 193 share a similar altitude band with ZHANGHENG 1.
❓ Frequently Asked Questions
ZHANGHENG 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 503 km altitude. Its 97.7° 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 95 minutes, travelling at 27,414 km/h.
ZHANGHENG 1 is operated by China Earthquake Administration/Italian Institute for Nuclear Physics (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43194. You can track ZHANGHENG 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
ZHANGHENG 1 was launched on 2018-02-02 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks ZHANGHENG 1 (NORAD ID 43194) 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.
ZHANGHENG 1 travels at approximately 27,414 km/h (17,034 mph) — roughly 7.61 km/s. It completes 15.21 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.