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Home Library Satellite Directory JILIN-01 KUANFU 02A

JILIN-01 KUANFU 02A

NORAD 57696 Payload LEO 2023-127A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
527 km
Apogee
542 km
Inclination
97.6°
Period
95.3 min
Mean Motion
15.10624966 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude535 km
Orbital Velocity27,351 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.11
Eccentricity0.0011
Semi-Major Axis6,906 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Chang Guang Satellite Technology (China)
Launch Date
2023-08-25
Launch Site
Jiuquan, China
Int'l Designator
2023-127A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
JILIN-01 KUANFU 02A is an active satellite operated by Chang Guang Satellite Technology (China), launched on 2023-08-25 from Jiuquan, China. It orbits in Low Earth Orbit (LEO) at altitudes between 527 km and 542 km with an inclination of 97.6°. It travels at approximately 27,351 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 KUANFU 02A 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 KUANFU 02A orbits at an average altitude of 535 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 KUANFU 02A’s average altitude, there are currently 3,509 active payloads and 312 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 20.1% of all active satellites. With an inclination of 97.6°, JILIN-01 KUANFU 02A passes over latitudes between 97.6°N and 97.6°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 207 share a similar altitude band with JILIN-01 KUANFU 02A.
❓ Frequently Asked Questions
JILIN-01 KUANFU 02A is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 535 km altitude. Its 97.6° 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 27,351 km/h.
JILIN-01 KUANFU 02A is operated by Chang Guang Satellite Technology (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 57696. You can track JILIN-01 KUANFU 02A in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
JILIN-01 KUANFU 02A was launched on 2023-08-25 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 KUANFU 02A (NORAD ID 57696) 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 KUANFU 02A travels at approximately 27,351 km/h (16,995 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.