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BEIJING 1

NORAD 28890 Payload LEO 2005-043A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
672 km
Apogee
692 km
Inclination
98.3°
Period
98.4 min
Mean Motion
14.63468554 rev/day
TLE Epoch
2026-03-17 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude682 km
Orbital Velocity27,064 km/h
Velocity7.52 km/s
Orbital Period98 minutes
Orbits / Day14.63
Eccentricity0.0014
Semi-Major Axis7,053 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2005-10-27
Launch Site
PKMTR
Int'l Designator
2005-043A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
🔗 Constellation / Groups
dmc
📖 About This Object
BEIJING 1 is an active satellite operated by China, launched on 2005-10-27 from PKMTR. With over 21 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 672 km and 692 km with an inclination of 98.3°. It travels at approximately 27,064 km/h (7.52 km/s), completing one full orbit every 98 minutes — that’s roughly 14.63 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. It is part of the Dmc constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks BEIJING 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
BEIJING 1 operates in a sun-synchronous orbit (SSO), a special subset of LEO where the orbital plane precesses to keep a constant angle relative to the Sun. This means the satellite crosses any given latitude at approximately the same local solar time on every pass, providing consistent lighting conditions — essential for Earth observation, weather monitoring and environmental science. SSO orbits typically sit between 600 and 800 km altitude with inclinations near 97–99°.
❓ Frequently Asked Questions
BEIJING 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 682 km altitude. Its 98.3° 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 98 minutes, travelling at 27,064 km/h.
BEIJING 1 is operated by China. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28890. You can track BEIJING 1 in real time on Orbital Radar’s live tracker.
BEIJING 1 was launched on 2005-10-27 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years.
Yes — Orbital Radar tracks BEIJING 1 (NORAD ID 28890) 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.
BEIJING 1 travels at approximately 27,064 km/h (16,816 mph) — roughly 7.52 km/s. It completes 14.63 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.
BEIJING 1 is a member of the Dmc constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Dmc satellites on Orbital Radar’s live tracker.