CZ-2D R/B
NORAD 68141
Rocket Body
LEO
2026-048C
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LEO · NORAD 68141
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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
569 km
Apogee
591 km
Inclination
35.1°
Period
96.3 min
Mean Motion
14.95795425 rev/day
TLE Epoch
2026-06-25 12:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude580 km
Orbital Velocity27,261 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.96
Eccentricity0.0016
Semi-Major Axis6,951 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-03-12
Launch Site
Xichang, China
Int'l Designator
2026-048C
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 2026-03-12 from Xichang, China on the Shiyan 30-03/04 launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Low Earth Orbit (LEO) at altitudes between 569 km and 591 km with an inclination of 35.1°. It travels at approximately 27,261 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.96 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. 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 580 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of CZ-2D R/B’s average altitude, there are currently 3,131 active payloads and 542 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 17.9% of all active satellites. With an inclination of 35.1°, CZ-2D R/B passes over latitudes between 35.1°N and 35.1°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. China operates approximately 1,221 active satellites in total, of which 184 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 orbits in Low Earth Orbit (LEO) at altitudes between 569 km (perigee) and 591 km (apogee), with an average altitude of approximately 580 km. It completes one orbit every 96 minutes, travelling at approximately 27,261 km/h (16,939 mph).
CZ-2D R/B (NORAD ID 68141) 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 2026-03-12 from Xichang, China. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-2D R/B (NORAD ID 68141) 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 27,261 km/h (16,939 mph) — roughly 7.57 km/s. It completes 14.96 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.