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JILIN-01 GAOFEN 3G

NORAD 46459 Payload LEO 2020-065F ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
258 km
Apogee
263 km
Inclination
97.2°
Period
89.7 min
Mean Motion
16.09506806 rev/day
TLE Epoch
2026-09-17 11:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude261 km
Orbital Velocity27,910 km/h
Velocity7.75 km/s
Orbital Period90 minutes
Orbits / Day16.10
Eccentricity0.0004
Semi-Major Axis6,632 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeWeeks to months
🚀 Launch & Identity
Country / Operator
🇨🇳 Chang Guang Satellite Technology Co. Ltd. (China)
Launch Date
2020-09-15
Launch Site
Yellow Sea launch area (Haiyang), China
Int'l Designator
2020-065F
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
JILIN-01 GAOFEN 3G is an active satellite operated by Chang Guang Satellite Technology Co. Ltd. (China), launched on 2020-09-15 from Yellow Sea launch area (Haiyang), China on the Jilin-1 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 258 km and 263 km with an inclination of 97.2°. It travels at approximately 27,910 km/h (7.75 km/s), completing one full orbit every 90 minutes — that’s roughly 16.10 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. 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 weeks to months. Orbital Radar tracks JILIN-01 GAOFEN 3G in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
JILIN-01 GAOFEN 3G orbits at an average altitude of 261 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of JILIN-01 GAOFEN 3G’s average altitude, there are currently 94 active payloads and 10 tracked debris or rocket body fragments — notable neighbours include STARLINK-1036, STARLINK-1067, STARLINK-1068. With an inclination of 97.2°, JILIN-01 GAOFEN 3G passes over latitudes between 97.2°N and 97.2°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 1,275 active satellites in total, of which 4 share a similar altitude band with JILIN-01 GAOFEN 3G.
❓ Frequently Asked Questions
JILIN-01 GAOFEN 3G is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 261 km altitude. Its 97.2° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 90 minutes, travelling at 27,910 km/h.
JILIN-01 GAOFEN 3G is operated by Chang Guang Satellite Technology Co. Ltd. (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 46459. You can track JILIN-01 GAOFEN 3G in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
JILIN-01 GAOFEN 3G was launched on 2020-09-15 from Yellow Sea launch area (Haiyang), China. At its current altitude, the estimated remaining orbital lifetime is: weeks to months. View the full satellite launch log.
Yes — Orbital Radar tracks JILIN-01 GAOFEN 3G (NORAD ID 46459) 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.
JILIN-01 GAOFEN 3G travels at approximately 27,910 km/h (17,343 mph) — roughly 7.75 km/s. It completes 16.10 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 32 sunrises and sunsets every 24 hours.