Skip to content
Home Library Satellite Directory CHUANG XIN 1-03

CHUANG XIN 1-03

NORAD 37930 Payload LEO 2011-068A ● Active
CONNECTING… LEO · NORAD 37930
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
778 km
Apogee
801 km
Inclination
98.7°
Period
100.7 min
Mean Motion
14.30537963 rev/day
TLE Epoch
2026-06-19 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude790 km
Orbital Velocity26,860 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.31
Eccentricity0.0016
Semi-Major Axis7,161 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Chinese Academy of Sciences (China)
Launch Date
2011-11-20
Launch Site
Jiuquan, China
Int'l Designator
2011-068A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CHUANG XIN 1-03 is an active satellite operated by Chinese Academy of Sciences (China), launched on 2011-11-20 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 778 km and 801 km with an inclination of 98.7°. It travels at approximately 26,860 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.31 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 ~25–100 years. Orbital Radar tracks CHUANG XIN 1-03 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CHUANG XIN 1-03 orbits at an average altitude of 790 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 CHUANG XIN 1-03’s average altitude, there are currently 421 active payloads and 2,242 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.7°, CHUANG XIN 1-03 passes over latitudes between 98.7°N and 98.7°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 95 share a similar altitude band with CHUANG XIN 1-03.
❓ Frequently Asked Questions
CHUANG XIN 1-03 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 790 km altitude. Its 98.7° 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 101 minutes, travelling at 26,860 km/h.
CHUANG XIN 1-03 is operated by Chinese Academy of Sciences (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 37930. You can track CHUANG XIN 1-03 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CHUANG XIN 1-03 was launched on 2011-11-20 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks CHUANG XIN 1-03 (NORAD ID 37930) 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.
CHUANG XIN 1-03 travels at approximately 26,860 km/h (16,690 mph) — roughly 7.46 km/s. It completes 14.31 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.