CBERS 2B
NORAD 32062
Payload
LEO
2007-042A
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LEO · NORAD 32062
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
732 km
Apogee
775 km
Inclination
98.4°
Period
99.9 min
Mean Motion
14.41476938 rev/day
TLE Epoch
2026-06-19 02:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude754 km
Orbital Velocity26,927 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.41
Eccentricity0.0030
Semi-Major Axis7,125 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
China/Brazil
Launch Date
2007-09-19
Launch Site
Taiyuan, China
Int'l Designator
2007-042A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
CBERS 2B is an active satellite operated by China/Brazil, launched on 2007-09-19 from Taiyuan, China. After 19 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 732 km and 775 km with an inclination of 98.4°. It travels at approximately 26,927 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.41 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 ~25–100 years. Orbital Radar tracks CBERS 2B 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 2B orbits at an average altitude of 754 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 2B’s average altitude, there are currently 354 active payloads and 1,990 tracked debris or rocket body fragments. With an inclination of 98.4°, CBERS 2B passes over latitudes between 98.4°N and 98.4°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 2B.
❓ Frequently Asked Questions
CBERS 2B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 754 km altitude. Its 98.4° 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 26,927 km/h.
CBERS 2B is operated by China/Brazil. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 32062. You can track CBERS 2B in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CBERS 2B was launched on 2007-09-19 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 2B (NORAD ID 32062) 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 2B travels at approximately 26,927 km/h (16,732 mph) — roughly 7.48 km/s. It completes 14.41 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.