JILIN-01 GAOFEN 2D
NORAD 49256
Payload
LEO
2021-086A
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LEO · NORAD 49256
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
510 km
Apogee
558 km
Inclination
97.7°
Period
95.3 min
Mean Motion
15.10659795 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude534 km
Orbital Velocity27,352 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.11
Eccentricity0.0035
Semi-Major Axis6,905 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Chang Guang Satellite Technology Co. Ltd. (China)
Launch Date
2021-09-27
Launch Site
Jiuquan, China
Int'l Designator
2021-086A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
JILIN-01 GAOFEN 2D is an active satellite operated by Chang Guang Satellite Technology Co. Ltd. (China), launched on 2021-09-27 from Jiuquan, China. It orbits in Low Earth Orbit (LEO) at altitudes between 510 km and 558 km with an inclination of 97.7°. It travels at approximately 27,352 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.11 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks JILIN-01 GAOFEN 2D 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 2D orbits at an average altitude of 534 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 2D’s average altitude, there are currently 3,514 active payloads and 305 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 20.2% of all active satellites. With an inclination of 97.7°, JILIN-01 GAOFEN 2D passes over latitudes between 97.7°N and 97.7°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 1,218 active satellites in total, of which 209 share a similar altitude band with JILIN-01 GAOFEN 2D.
❓ Frequently Asked Questions
JILIN-01 GAOFEN 2D is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 534 km altitude. Its 97.7° 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 95 minutes, travelling at 27,352 km/h.
JILIN-01 GAOFEN 2D is operated by Chang Guang Satellite Technology Co. Ltd. (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 49256. You can track JILIN-01 GAOFEN 2D in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
JILIN-01 GAOFEN 2D was launched on 2021-09-27 from Jiuquan, China, one of China’s oldest launch centres in the Gobi Desert, used for crewed Shenzhou missions and LEO satellites. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks JILIN-01 GAOFEN 2D (NORAD ID 49256) 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 2D travels at approximately 27,352 km/h (16,996 mph) — roughly 7.60 km/s. It completes 15.11 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.