CHUANG XIN 16A (CX-16A)
NORAD 53586
Payload
LEO
2022-102A
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Altitude (km)
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Longitude
🛰️ Orbital Parameters
Perigee
545 km
Apogee
552 km
Inclination
29.0°
Period
95.6 min
Mean Motion
15.05934455 rev/day
TLE Epoch
2026-06-18 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude549 km
Orbital Velocity27,323 km/h
Velocity7.59 km/s
Orbital Period96 minutes
Orbits / Day15.06
Eccentricity0.0005
Semi-Major Axis6,920 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Chinese Academy of Sciences (China)
Launch Date
2022-08-23
Launch Site
Xichang, China
Int'l Designator
2022-102A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
CHUANG XIN 16A (CX-16A) is an active satellite operated by Chinese Academy of Sciences (China), launched on 2022-08-23 from Xichang, China. It orbits in Low Earth Orbit (LEO) at altitudes between 545 km and 552 km with an inclination of 29.0°. It travels at approximately 27,323 km/h (7.59 km/s), completing one full orbit every 96 minutes — that’s roughly 15.06 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 ~3–10 years. Orbital Radar tracks CHUANG XIN 16A (CX-16A) 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 16A (CX-16A) orbits at an average altitude of 549 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of CHUANG XIN 16A (CX-16A)’s average altitude, there are currently 3,461 active payloads and 359 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, ONEWEB-0050. This makes it one of the more crowded altitude bands, containing roughly 19.9% of all active satellites. With an inclination of 29.0°, CHUANG XIN 16A (CX-16A) passes over latitudes between 29.0°N and 29.0°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 1,219 active satellites in total, of which 163 share a similar altitude band with CHUANG XIN 16A (CX-16A).
❓ Frequently Asked Questions
CHUANG XIN 16A (CX-16A) orbits in Low Earth Orbit (LEO) at altitudes between 545 km (perigee) and 552 km (apogee), with an average altitude of approximately 549 km. It completes one orbit every 96 minutes, travelling at approximately 27,323 km/h (16,978 mph).
CHUANG XIN 16A (CX-16A) is operated by Chinese Academy of Sciences (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 53586. You can track CHUANG XIN 16A (CX-16A) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CHUANG XIN 16A (CX-16A) was launched on 2022-08-23 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks CHUANG XIN 16A (CX-16A) (NORAD ID 53586) 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 16A (CX-16A) travels at approximately 27,323 km/h (16,978 mph) — roughly 7.59 km/s. It completes 15.06 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.