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CBERS 1

NORAD 25940 Payload LEO 1999-057A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
765 km
Apogee
772 km
Inclination
98.8°
Period
100.2 min
Mean Motion
14.37005069 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude769 km
Orbital Velocity26,899 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.37
Eccentricity0.0005
Semi-Major Axis7,140 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
China/Brazil
Launch Date
1999-10-14
Launch Site
Taiyuan, China
Int'l Designator
1999-057A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
CBERS 1 is an active satellite operated by China/Brazil, launched on 1999-10-14 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 765 km and 772 km with an inclination of 98.8°. It travels at approximately 26,899 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.37 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 ~25–100 years. Orbital Radar tracks CBERS 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
CBERS 1 orbits at an average altitude of 769 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 CBERS 1’s average altitude, there are currently 382 active payloads and 2,084 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179, ONEWEB-0455. With an inclination of 98.8°, CBERS 1 passes over latitudes between 98.8°N and 98.8°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/Brazil operates approximately 4 active satellites in total, of which 3 share a similar altitude band with CBERS 1.
❓ Frequently Asked Questions
CBERS 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 769 km altitude. Its 98.8° 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 100 minutes, travelling at 26,899 km/h.
CBERS 1 is operated by China/Brazil. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25940. You can track CBERS 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CBERS 1 was launched on 1999-10-14 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks CBERS 1 (NORAD ID 25940) 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.
CBERS 1 travels at approximately 26,899 km/h (16,714 mph) — roughly 7.47 km/s. It completes 14.37 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.