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QIANFAN-174

NORAD 69391 Payload LEO 2026-124K ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
820 km
Apogee
825 km
Inclination
89.0°
Period
101.3 min
Mean Motion
14.20879570 rev/day
TLE Epoch
2026-06-26 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude823 km
Orbital Velocity26,798 km/h
Velocity7.44 km/s
Orbital Period101 minutes
Orbits / Day14.21
Eccentricity0.0003
Semi-Major Axis7,194 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-06-04
Launch Site
Taiyuan, China
Int'l Designator
2026-124K
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
qianfan
📖 About This Object
QIANFAN-174 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 820 km and 825 km with an inclination of 89.0°. It travels at approximately 26,798 km/h (7.44 km/s), completing one full orbit every 101 minutes — that’s roughly 14.21 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-174 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-174 orbits at an average altitude of 823 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-174’s average altitude, there are currently 380 active payloads and 2,275 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 89.0°, QIANFAN-174 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 112 share a similar altitude band with QIANFAN-174.
❓ Frequently Asked Questions
QIANFAN-174 orbits in Low Earth Orbit (LEO) at altitudes between 820 km (perigee) and 825 km (apogee), with an average altitude of approximately 823 km. It completes one orbit every 101 minutes, travelling at approximately 26,798 km/h (16,651 mph).
QIANFAN-174 is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 69391. You can track QIANFAN-174 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
QIANFAN-174 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-174 (NORAD ID 69391) 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-174 travels at approximately 26,798 km/h (16,651 mph) — roughly 7.44 km/s. It completes 14.21 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.
QIANFAN-174 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.