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Home Library Satellite Directory SJ-11-03

SJ-11-03

NORAD 37730 Payload LEO 2011-030A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
673 km
Apogee
686 km
Inclination
97.9°
Period
98.3 min
Mean Motion
14.64337988 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude680 km
Orbital Velocity27,068 km/h
Velocity7.52 km/s
Orbital Period98 minutes
Orbits / Day14.64
Eccentricity0.0009
Semi-Major Axis7,051 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China Academy of Space Technology (CAST) (China)
Launch Date
2011-07-06
Launch Site
Jiuquan, China
Int'l Designator
2011-030A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SJ-11-03 is an active satellite operated by China Academy of Space Technology (CAST) (China), launched on 2011-07-06 from Jiuquan, China. After 15 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 673 km and 686 km with an inclination of 97.9°. It travels at approximately 27,068 km/h (7.52 km/s), completing one full orbit every 98 minutes — that’s roughly 14.64 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 SJ-11-03 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SJ-11-03 orbits at an average altitude of 680 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 SJ-11-03’s average altitude, there are currently 330 active payloads and 1,268 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 97.9°, SJ-11-03 passes over latitudes between 97.9°N and 97.9°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 1,219 active satellites in total, of which 72 share a similar altitude band with SJ-11-03.
❓ Frequently Asked Questions
SJ-11-03 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 680 km altitude. Its 97.9° 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 27,068 km/h.
SJ-11-03 is operated by China Academy of Space Technology (CAST) (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 37730. You can track SJ-11-03 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SJ-11-03 was launched on 2011-07-06 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 SJ-11-03 (NORAD ID 37730) 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.
SJ-11-03 travels at approximately 27,068 km/h (16,819 mph) — roughly 7.52 km/s. It completes 14.64 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.