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JILIN-01-04

NORAD 43022 Payload LEO 2017-074A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
431 km
Apogee
435 km
Inclination
97.5°
Period
93.2 min
Mean Motion
15.44627325 rev/day
TLE Epoch
2026-09-17 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude433 km
Orbital Velocity27,554 km/h
Velocity7.65 km/s
Orbital Period93 minutes
Orbits / Day15.45
Eccentricity0.0003
Semi-Major Axis6,804 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Chang Guang Satellite Technology Co. Ltd. (China)
Launch Date
2017-11-21
Launch Site
Taiyuan Satellite Launch Center, China
Int'l Designator
2017-074A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
JILIN-01-04 is an active satellite operated by Chang Guang Satellite Technology Co. Ltd. (China), launched on 2017-11-21 from Taiyuan Satellite Launch Center, China on the Jilin-1 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 431 km and 435 km with an inclination of 97.5°. It travels at approximately 27,554 km/h (7.65 km/s), completing one full orbit every 93 minutes — that’s roughly 15.45 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 ~1–3 years. Orbital Radar tracks JILIN-01-04 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-01-04 orbits at an average altitude of 433 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-01-04’s average altitude, there are currently 9,577 active payloads and 122 tracked debris or rocket body fragments — notable neighbours include ISS (ZARYA), STARLINK-1017, STARLINK-1039. This makes it one of the more crowded altitude bands, containing roughly 51.2% of all active satellites. With an inclination of 97.5°, JILIN-01-04 passes over latitudes between 97.5°N and 97.5°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 76 share a similar altitude band with JILIN-01-04.
❓ Frequently Asked Questions
JILIN-01-04 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 433 km altitude. Its 97.5° 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 93 minutes, travelling at 27,554 km/h.
JILIN-01-04 is operated by Chang Guang Satellite Technology Co. Ltd. (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 43022. You can track JILIN-01-04 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
JILIN-01-04 was launched on 2017-11-21 from Taiyuan Satellite Launch Center, China. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks JILIN-01-04 (NORAD ID 43022) 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-01-04 travels at approximately 27,554 km/h (17,121 mph) — roughly 7.65 km/s. It completes 15.45 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.