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TANSUO 1

NORAD 28220 Payload LEO 2004-012A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
461 km
Apogee
468 km
Inclination
97.9°
Period
93.9 min
Mean Motion
15.33804033 rev/day
TLE Epoch
2026-06-19 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude465 km
Orbital Velocity27,491 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.34
Eccentricity0.0005
Semi-Major Axis6,836 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China Academy of Space Technology (CAST) (China)
Launch Date
2004-04-18
Launch Site
Xichang, China
Int'l Designator
2004-012A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
TANSUO 1 is an active satellite operated by China Academy of Space Technology (CAST) (China), launched on 2004-04-18 from Xichang, China. With over 22 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 461 km and 468 km with an inclination of 97.9°. It travels at approximately 27,491 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.34 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 TANSUO 1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
TANSUO 1 orbits at an average altitude of 465 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 TANSUO 1’s average altitude, there are currently 7,997 active payloads and 179 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1017. This makes it one of the more crowded altitude bands, containing roughly 45.9% of all active satellites. With an inclination of 97.9°, TANSUO 1 passes over latitudes between 97.9°N and 97.9°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 1,219 active satellites in total, of which 164 share a similar altitude band with TANSUO 1.
❓ Frequently Asked Questions
TANSUO 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 465 km altitude. Its 97.9° 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 94 minutes, travelling at 27,491 km/h.
TANSUO 1 is operated by China Academy of Space Technology (CAST) (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28220. You can track TANSUO 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
TANSUO 1 was launched on 2004-04-18 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks TANSUO 1 (NORAD ID 28220) 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.
TANSUO 1 travels at approximately 27,491 km/h (17,082 mph) — roughly 7.64 km/s. It completes 15.34 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.