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FALCON 9 R/B

NORAD 47307 Rocket Body HEO 2021-001B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
273 km
Apogee
47383 km
Inclination
15.5°
Period
870.8 min
Mean Motion
1.65377653 rev/day
TLE Epoch
2026-06-25 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude23,828 km
Orbital Velocity13,079 km/h
Velocity3.63 km/s
Orbital Period14 hours 31 minutes
Orbits / Day1.65
Eccentricity0.7800
Semi-Major Axis30,199 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2021-01-08
Launch Site
Cape Canaveral, Florida
Int'l Designator
2021-001B
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 2021-01-08 from Cape Canaveral, Florida on the Turksat 5A launch. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 273 km and 47,383 km with an inclination of 15.5°. It travels at approximately 13,079 km/h (3.63 km/s), completing one full orbit every 14 hours 31 minutes — that’s roughly 1.65 orbits per day. Its orbital eccentricity of 0.7800 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. 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 follows a Highly Elliptical Orbit, sweeping between 273 km (perigee) and 47,383 km (apogee). It spends most of its 14 hours 31 minutes orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. Within ±50 km of FALCON 9 R/B’s average altitude, there are currently 2 active payloads and 2 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 15.5°, FALCON 9 R/B passes over latitudes between 15.5°N and 15.5°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. United States operates approximately 12,413 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 follows a Highly Elliptical Orbit, swinging between 273 km (perigee) and 47,383 km (apogee). It spends most of its 14 hours 31 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
FALCON 9 R/B (NORAD ID 47307) 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 2021-01-08 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. 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 FALCON 9 R/B (NORAD ID 47307) 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’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 13,079 km/h (3.63 km/s), completing one revolution every 14 hours 31 minutes. Learn more about highly elliptical orbits.