LQSAT
NORAD 40958
Payload
LEO
2015-057A
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LEO · NORAD 40958
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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
629 km
Apogee
650 km
Inclination
97.7°
Period
97.5 min
Mean Motion
14.76785212 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude640 km
Orbital Velocity27,145 km/h
Velocity7.54 km/s
Orbital Period98 minutes
Orbits / Day14.77
Eccentricity0.0015
Semi-Major Axis7,011 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Changchun Institute of Optics (China)
Launch Date
2015-10-07
Launch Site
Jiuquan, China
Int'l Designator
2015-057A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LQSAT is an active satellite operated by Changchun Institute of Optics (China), launched on 2015-10-07 from Jiuquan, China. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 629 km and 650 km with an inclination of 97.7°. It travels at approximately 27,145 km/h (7.54 km/s), completing one full orbit every 98 minutes — that’s roughly 14.77 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 ~10–25 years. Orbital Radar tracks LQSAT in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
LQSAT orbits at an average altitude of 640 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 LQSAT’s average altitude, there are currently 742 active payloads and 930 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0050. With an inclination of 97.7°, LQSAT 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 1,218 active satellites in total, of which 155 share a similar altitude band with LQSAT.
❓ Frequently Asked Questions
LQSAT is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 640 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 98 minutes, travelling at 27,145 km/h.
LQSAT is operated by Changchun Institute of Optics (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 40958. You can track LQSAT in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
LQSAT was launched on 2015-10-07 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: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks LQSAT (NORAD ID 40958) 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.
LQSAT travels at approximately 27,145 km/h (16,867 mph) — roughly 7.54 km/s. It completes 14.77 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.