CHUANG XIN 26 (CX-26)
NORAD 69972
Payload
LEO
2026-158A
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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
804 km
Apogee
812 km
Inclination
50.0°
Period
101.0 min
Mean Motion
14.25145244 rev/day
TLE Epoch
2026-07-11 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude808 km
Orbital Velocity26,825 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.25
Eccentricity0.0006
Semi-Major Axis7,179 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-07-10
Launch Site
Wenchang, China
Int'l Designator
2026-158A
Object Type
Payload
RCS Size
Unknown
📖 About This Object
CHUANG XIN 26 (CX-26) is an active satellite operated by China, launched on 2026-07-10 from Wenchang, China on the CX-26 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 804 km and 812 km with an inclination of 50.0°. It travels at approximately 26,825 km/h (7.45 km/s), completing one full orbit every 101 minutes — that’s roughly 14.25 orbits per day. 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 ~100–500 years. Orbital Radar tracks CHUANG XIN 26 (CX-26) 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 26 (CX-26) orbits at an average altitude of 808 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of CHUANG XIN 26 (CX-26)’s average altitude, there are currently 403 active payloads and 2,313 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 50.0°, CHUANG XIN 26 (CX-26) passes over latitudes between 50.0°N and 50.0°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. China operates approximately 1,213 active satellites in total, of which 69 share a similar altitude band with CHUANG XIN 26 (CX-26).
❓ Frequently Asked Questions
CHUANG XIN 26 (CX-26) orbits in Low Earth Orbit (LEO) at altitudes between 804 km (perigee) and 812 km (apogee), with an average altitude of approximately 808 km. It completes one orbit every 101 minutes, travelling at approximately 26,825 km/h (16,668 mph).
CHUANG XIN 26 (CX-26) is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 69972. You can track CHUANG XIN 26 (CX-26) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CHUANG XIN 26 (CX-26) was launched on 2026-07-10 from Wenchang, China, China’s newest coastal launch facility on Hainan Island, used for heavy-lift Long March 5 missions. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks CHUANG XIN 26 (CX-26) (NORAD ID 69972) 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 26 (CX-26) travels at approximately 26,825 km/h (16,668 mph) — roughly 7.45 km/s. It completes 14.25 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.