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YAOGAN-40 04A

NORAD 100823 Payload LEO 2026-222A ● Active
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🛰️ Orbital Parameters
Perigee
773 km
Apogee
792 km
Inclination
86.0°
Period
100.5 min
Mean Motion
14.32667627 rev/day
TLE Epoch
2026-10-06 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude783 km
Orbital Velocity26,873 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.33
Eccentricity0.0013
Semi-Major Axis7,154 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 PLA Strategic Support Force (China)
Launch Date
2026-09-24
Launch Site
Taiyuan Satellite Launch Center, China
Int'l Designator
2026-222A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
YAOGAN-40 04A is an active satellite operated by PLA Strategic Support Force (China), launched on 2026-09-24 from Taiyuan Satellite Launch Center, China on the Yaogan 40-04 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 773 km and 792 km with an inclination of 86.0°. It travels at approximately 26,873 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.33 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks YAOGAN-40 04A in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
YAOGAN-40 04A orbits at an average altitude of 783 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of YAOGAN-40 04A’s average altitude, there are currently 444 active payloads and 2,453 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0455. With an inclination of 86.0°, YAOGAN-40 04A passes over latitudes between 86.0°N and 86.0°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 1,323 active satellites in total, of which 65 share a similar altitude band with YAOGAN-40 04A.
🔗 Yaogan Reconnaissance Series

This satellite is part of China's Yaogan series, officially described as “remote sensing” satellites but widely assessed by analysts to serve military reconnaissance, signals intelligence and ocean surveillance missions. The series includes optical imaging, synthetic aperture radar (SAR) and electronic intelligence (ELINT) variants, some operating in coordinated orbital formations for persistent maritime monitoring.

❓ Frequently Asked Questions
YAOGAN-40 04A orbits in Low Earth Orbit (LEO) at altitudes between 773 km (perigee) and 792 km (apogee), with an average altitude of approximately 783 km. It completes one orbit every 101 minutes, travelling at approximately 26,873 km/h (16,698 mph).
YAOGAN-40 04A is operated by PLA Strategic Support Force (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 100823. You can track YAOGAN-40 04A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YAOGAN-40 04A was launched on 2026-09-24 from Taiyuan Satellite Launch Center, China. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks YAOGAN-40 04A (NORAD ID 100823) 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.
YAOGAN-40 04A travels at approximately 26,873 km/h (16,698 mph) — roughly 7.46 km/s. It completes 14.33 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.