CZ-7A R/B
NORAD 69675
Rocket Body
MEO
2026-144B
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MEO · NORAD 69675
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
102 km
Apogee
9032 km
Inclination
19.4°
Period
189.9 min
Mean Motion
7.58167250 rev/day
TLE Epoch
2026-09-04 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude4,567 km
Orbital Velocity21,732 km/h
Velocity6.04 km/s
Orbital Period3 hours 10 minutes
Orbits / Day7.58
Eccentricity0.4082
Semi-Major Axis10,938 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2026-06-23
Launch Site
Wenchang, China
Int'l Designator
2026-144B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
CZ-7A R/B is a spent rocket body associated with China, launched on 2026-06-23 from Wenchang, China on the TJS-26A launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Medium Earth Orbit (MEO) at altitudes between 102 km and 9,032 km with an inclination of 19.4°. It travels at approximately 21,732 km/h (6.04 km/s), completing one full orbit every 3 hours 10 minutes — that’s roughly 7.58 orbits per day. Its orbital eccentricity of 0.4082 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like CZ-7A 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-7A R/B orbits at an average altitude of 4,567 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. With an inclination of 19.4°, CZ-7A R/B passes over latitudes between 19.4°N and 19.4°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. China operates approximately 1,276 active satellites in total.
🔗 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-7A R/B orbits in Medium Earth Orbit (MEO) at altitudes between 102 km (perigee) and 9,032 km (apogee), with an average altitude of approximately 4,567 km. It completes one orbit every 3 hours 10 minutes, travelling at approximately 21,732 km/h (13,504 mph).
CZ-7A R/B (NORAD ID 69675) 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-7A R/B was launched on 2026-06-23 from Wenchang, China, China’s newest coastal launch facility on Hainan Island, used for heavy-lift Long March 5 missions. At its current altitude, the estimated remaining orbital lifetime is: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks CZ-7A R/B (NORAD ID 69675) 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-7A R/B travels at approximately 21,732 km/h (13,504 mph) — roughly 6.04 km/s. It completes 7.58 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 15 sunrises and sunsets every 24 hours.