QIANFAN-169
NORAD 69386
Payload
LEO
2026-124E
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LEO · NORAD 69386
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Altitude (km)
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🛰️ Orbital Parameters
Perigee
828 km
Apogee
834 km
Inclination
89.0°
Period
101.5 min
Mean Motion
14.18287956 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude831 km
Orbital Velocity26,782 km/h
Velocity7.44 km/s
Orbital Period102 minutes
Orbits / Day14.18
Eccentricity0.0004
Semi-Major Axis7,202 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-06-04
Launch Site
Taiyuan, China
Int'l Designator
2026-124E
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
qianfan
📖 About This Object
QIANFAN-169 is an active satellite operated by China, launched on 2026-06-04 from Taiyuan, China on the Qianfan Jigui 11 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 828 km and 834 km with an inclination of 89.0°. It travels at approximately 26,782 km/h (7.44 km/s), completing one full orbit every 102 minutes — that’s roughly 14.18 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. It is part of the Qianfan constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks QIANFAN-169 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
QIANFAN-169 orbits at an average altitude of 831 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 QIANFAN-169’s average altitude, there are currently 277 active payloads and 2,211 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 89.0°, QIANFAN-169 passes over latitudes between 89.0°N and 89.0°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 1,221 active satellites in total, of which 106 share a similar altitude band with QIANFAN-169.
❓ Frequently Asked Questions
QIANFAN-169 orbits in Low Earth Orbit (LEO) at altitudes between 828 km (perigee) and 834 km (apogee), with an average altitude of approximately 831 km. It completes one orbit every 102 minutes, travelling at approximately 26,782 km/h (16,642 mph).
QIANFAN-169 is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 69386. You can track QIANFAN-169 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
QIANFAN-169 was launched on 2026-06-04 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks QIANFAN-169 (NORAD ID 69386) 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.
QIANFAN-169 travels at approximately 26,782 km/h (16,642 mph) — roughly 7.44 km/s. It completes 14.18 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.
QIANFAN-169 is a member of the Qianfan constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Qianfan satellites on Orbital Radar’s live tracker.