Skip to content
Home Library Satellite Directory CHUANG XIN 1 (CZ-1)

CHUANG XIN 1 (CZ-1)

NORAD 28058 Payload LEO 2003-049B ● Active
CONNECTING… LEO · NORAD 28058
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
721 km
Apogee
739 km
Inclination
98.5°
Period
99.4 min
Mean Motion
14.48585331 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude730 km
Orbital Velocity26,972 km/h
Velocity7.49 km/s
Orbital Period99 minutes
Orbits / Day14.49
Eccentricity0.0013
Semi-Major Axis7,101 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Chinese Academy of Sciences (China)
Launch Date
2003-10-21
Launch Site
Taiyuan, China
Int'l Designator
2003-049B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CHUANG XIN 1 (CZ-1) is an active satellite operated by Chinese Academy of Sciences (China), launched on 2003-10-21 from Taiyuan, China. With over 23 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 721 km and 739 km with an inclination of 98.5°. It travels at approximately 26,972 km/h (7.49 km/s), completing one full orbit every 99 minutes — that’s roughly 14.49 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 (CZ-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
CHUANG XIN 1 (CZ-1) orbits at an average altitude of 730 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 (CZ-1)’s average altitude, there are currently 360 active payloads and 1,843 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.5°, CHUANG XIN 1 (CZ-1) passes over latitudes between 98.5°N and 98.5°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 50 share a similar altitude band with CHUANG XIN 1 (CZ-1).
❓ Frequently Asked Questions
CHUANG XIN 1 (CZ-1) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 730 km altitude. Its 98.5° 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 99 minutes, travelling at 26,972 km/h.
CHUANG XIN 1 (CZ-1) is operated by Chinese Academy of Sciences (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28058. You can track CHUANG XIN 1 (CZ-1) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CHUANG XIN 1 (CZ-1) was launched on 2003-10-21 from Taiyuan, China. 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 (CZ-1) (NORAD ID 28058) 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 (CZ-1) travels at approximately 26,972 km/h (16,760 mph) — roughly 7.49 km/s. It completes 14.49 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.