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CZ-2D R/B

NORAD 28738 Rocket Body LEO 2005-024B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
357 km
Apogee
359 km
Inclination
97.3°
Period
91.7 min
Mean Motion
15.70498789 rev/day
TLE Epoch
2026-06-26 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude358 km
Orbital Velocity27,707 km/h
Velocity7.70 km/s
Orbital Period92 minutes
Orbits / Day15.70
Eccentricity0.0001
Semi-Major Axis6,729 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital LifetimeMonths to ~1 year
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2005-07-05
Launch Site
Jiuquan, China
Int'l Designator
2005-024B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-2D R/B is a spent rocket body associated with China, launched on 2005-07-05 from Jiuquan, China on the Tansuo-2 launch. With over 21 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 357 km and 359 km with an inclination of 97.3°. It travels at approximately 27,707 km/h (7.70 km/s), completing one full orbit every 92 minutes — that’s roughly 15.70 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 months to ~1 year. Spent rocket bodies like CZ-2D R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
CZ-2D R/B orbits at an average altitude of 358 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 CZ-2D R/B’s average altitude, there are currently 1,190 active payloads and 52 tracked debris or rocket body fragments — notable neighbours include STARLINK-1020, STARLINK-1036, STARLINK-1042. This makes it one of the more crowded altitude bands, containing roughly 6.8% of all active satellites. With an inclination of 97.3°, CZ-2D R/B passes over latitudes between 97.3°N and 97.3°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 1,221 active satellites in total, of which 23 share a similar altitude band with CZ-2D R/B.
🔗 Spent Rocket Body

This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.

❓ Frequently Asked Questions
CZ-2D R/B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 358 km altitude. Its 97.3° 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 92 minutes, travelling at 27,707 km/h.
CZ-2D R/B (NORAD ID 28738) is a spent rocket body — the upper stage of a launch vehicle attributed to China. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
CZ-2D R/B was launched on 2005-07-05 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: months to ~1 year. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-2D R/B (NORAD ID 28738) 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.
CZ-2D R/B travels at approximately 27,707 km/h (17,217 mph) — roughly 7.70 km/s. It completes 15.70 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.