Skip to content
Home Library Satellite Directory CZ-7A R/B

CZ-7A R/B

NORAD 67303 Rocket Body MEO 2025-315B
CONNECTING… MEO · NORAD 67303
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
199 km
Apogee
32751 km
Inclination
19.8°
Period
573.0 min
Mean Motion
2.51294717 rev/day
TLE Epoch
2026-06-24 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude16,475 km
Orbital Velocity15,037 km/h
Velocity4.18 km/s
Orbital Period9 hours 33 minutes
Orbits / Day2.51
Eccentricity0.7124
Semi-Major Axis22,846 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇨🇳 China
Launch Date
2025-12-30
Launch Site
Wenchang, China
Int'l Designator
2025-315B
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 2025-12-30 from Wenchang, China on the Shijian 29A/B 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 199 km and 32,751 km with an inclination of 19.8°. It travels at approximately 15,037 km/h (4.18 km/s), completing one full orbit every 9 hours 33 minutes — that’s roughly 2.51 orbits per day. Its orbital eccentricity of 0.7124 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 16,475 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. Within ±50 km of CZ-7A R/B’s average altitude, there are currently 0 active payloads and 8 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 19.8°, CZ-7A R/B passes over latitudes between 19.8°N and 19.8°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. China operates approximately 1,221 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 199 km (perigee) and 32,751 km (apogee), with an average altitude of approximately 16,475 km. It completes one orbit every 9 hours 33 minutes, travelling at approximately 15,037 km/h (9,344 mph).
CZ-7A R/B (NORAD ID 67303) 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 2025-12-30 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 67303) 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 15,037 km/h (9,344 mph) — roughly 4.18 km/s. It completes 2.51 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 5 sunrises and sunsets every 24 hours.