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YUNHAI 2-2E

NORAD 59284 Payload LEO 2024-052E ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
790 km
Apogee
807 km
Inclination
50.0°
Period
100.8 min
Mean Motion
14.27965275 rev/day
TLE Epoch
2026-06-19 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude799 km
Orbital Velocity26,843 km/h
Velocity7.46 km/s
Orbital Period101 minutes
Orbits / Day14.28
Eccentricity0.0012
Semi-Major Axis7,170 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2024-03-21
Launch Site
Jiuquan, China
Int'l Designator
2024-052E
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
YUNHAI 2-2E is an active satellite operated by China, launched on 2024-03-21 from Jiuquan, China. It orbits in Low Earth Orbit (LEO) at altitudes between 790 km and 807 km with an inclination of 50.0°. It travels at approximately 26,843 km/h (7.46 km/s), completing one full orbit every 101 minutes — that’s roughly 14.28 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks YUNHAI 2-2E in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
YUNHAI 2-2E orbits at an average altitude of 799 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of YUNHAI 2-2E’s average altitude, there are currently 434 active payloads and 2,269 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 50.0°, YUNHAI 2-2E passes over latitudes between 50.0°N and 50.0°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. China operates approximately 1,219 active satellites in total, of which 96 share a similar altitude band with YUNHAI 2-2E.
❓ Frequently Asked Questions
YUNHAI 2-2E orbits in Low Earth Orbit (LEO) at altitudes between 790 km (perigee) and 807 km (apogee), with an average altitude of approximately 799 km. It completes one orbit every 101 minutes, travelling at approximately 26,843 km/h (16,679 mph).
YUNHAI 2-2E is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 59284. You can track YUNHAI 2-2E in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
YUNHAI 2-2E was launched on 2024-03-21 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks YUNHAI 2-2E (NORAD ID 59284) 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.
YUNHAI 2-2E travels at approximately 26,843 km/h (16,679 mph) — roughly 7.46 km/s. It completes 14.28 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.