FALCON 9 R/B
NORAD 61184
Rocket Body
MEO
2024-167C
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MEO · NORAD 61184
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
22946 km
Apogee
23008 km
Inclination
55.2°
Period
834.2 min
Mean Motion
1.72615443 rev/day
TLE Epoch
2026-07-15 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude22,977 km
Orbital Velocity13,267 km/h
Velocity3.69 km/s
Orbital Period13 hours 54 minutes
Orbits / Day1.73
Eccentricity0.0011
Semi-Major Axis29,348 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2024-09-17
Launch Site
Cape Canaveral, Florida
Int'l Designator
2024-167C
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
FALCON 9 R/B is a spent rocket body associated with United States, launched on 2024-09-17 from Cape Canaveral, Florida on the Galileo L13 launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 22,946 km and 23,008 km with an inclination of 55.2°. It travels at approximately 13,267 km/h (3.69 km/s), completing one full orbit every 13 hours 54 minutes — that’s roughly 1.73 orbits per day. Spent rocket bodies like FALCON 9 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
FALCON 9 R/B orbits at an average altitude of 22,977 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 FALCON 9 R/B’s average altitude, there are currently 0 active payloads and 3 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 55.2°, FALCON 9 R/B passes over latitudes between 55.2°N and 55.2°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 12,511 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
FALCON 9 R/B orbits in Medium Earth Orbit (MEO) at altitudes between 22,946 km (perigee) and 23,008 km (apogee), with an average altitude of approximately 22,977 km. It completes one orbit every 13 hours 54 minutes, travelling at approximately 13,267 km/h (8,244 mph).
FALCON 9 R/B (NORAD ID 61184) is a spent rocket body — the upper stage of a launch vehicle attributed to United States. 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.
FALCON 9 R/B was launched on 2024-09-17 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks FALCON 9 R/B (NORAD ID 61184) 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.
FALCON 9 R/B travels at approximately 13,267 km/h (8,244 mph) — roughly 3.69 km/s. It completes 1.73 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 3 sunrises and sunsets every 24 hours.