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SJ-5

NORAD 25731 Payload LEO 1999-025B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
837 km
Apogee
861 km
Inclination
98.7°
Period
101.9 min
Mean Motion
14.12931508 rev/day
TLE Epoch
2026-06-19 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude849 km
Orbital Velocity26,749 km/h
Velocity7.43 km/s
Orbital Period102 minutes
Orbits / Day14.13
Eccentricity0.0017
Semi-Major Axis7,220 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
1999-05-10
Launch Site
Taiyuan, China
Int'l Designator
1999-025B
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SJ-5 is an active satellite operated by China, launched on 1999-05-10 from Taiyuan, China. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 837 km and 861 km with an inclination of 98.7°. It travels at approximately 26,749 km/h (7.43 km/s), completing one full orbit every 102 minutes — that’s roughly 14.13 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 ~100–500 years. Orbital Radar tracks SJ-5 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SJ-5 orbits at an average altitude of 849 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 SJ-5’s average altitude, there are currently 249 active payloads and 2,064 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.7°, SJ-5 passes over latitudes between 98.7°N and 98.7°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 119 share a similar altitude band with SJ-5.
🔗 Fengyun-1C ASAT Debris

This debris object was created by China's kinetic-kill anti-satellite test on 11 January 2007, which destroyed the Fengyun-1C weather satellite at approximately 865 km altitude. The test generated over 3,500 trackable fragments — the worst debris event in spaceflight history — with debris expected to persist in orbit for decades to centuries due to the high altitude. About 2,800 fragments remain catalogued as of 2026.

❓ Frequently Asked Questions
SJ-5 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 849 km altitude. Its 98.7° 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 102 minutes, travelling at 26,749 km/h.
SJ-5 is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25731. You can track SJ-5 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SJ-5 was launched on 1999-05-10 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 SJ-5 (NORAD ID 25731) 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.
SJ-5 travels at approximately 26,749 km/h (16,621 mph) — roughly 7.43 km/s. It completes 14.13 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.