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QIANFAN-168

NORAD 69385 Payload LEO 2026-124D ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
830 km
Apogee
835 km
Inclination
89.0°
Period
101.6 min
Mean Motion
14.17874163 rev/day
TLE Epoch
2026-06-25 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude833 km
Orbital Velocity26,779 km/h
Velocity7.44 km/s
Orbital Period102 minutes
Orbits / Day14.18
Eccentricity0.0003
Semi-Major Axis7,204 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-06-04
Launch Site
Taiyuan, China
Int'l Designator
2026-124D
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
qianfan
📖 About This Object
QIANFAN-168 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 830 km and 835 km with an inclination of 89.0°. It travels at approximately 26,779 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-168 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-168 orbits at an average altitude of 833 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-168’s average altitude, there are currently 270 active payloads and 2,206 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 89.0°, QIANFAN-168 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 105 share a similar altitude band with QIANFAN-168.
❓ Frequently Asked Questions
QIANFAN-168 orbits in Low Earth Orbit (LEO) at altitudes between 830 km (perigee) and 835 km (apogee), with an average altitude of approximately 833 km. It completes one orbit every 102 minutes, travelling at approximately 26,779 km/h (16,640 mph).
QIANFAN-168 is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 69385. You can track QIANFAN-168 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
QIANFAN-168 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-168 (NORAD ID 69385) 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-168 travels at approximately 26,779 km/h (16,640 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-168 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.