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FALCON 9 R/B

NORAD 62484 Rocket Body HEO 2025-001B
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🛰️ Orbital Parameters
Perigee
404 km
Apogee
53780 km
Inclination
24.2°
Period
1015.7 min
Mean Motion
1.41780576 rev/day
TLE Epoch
2026-10-15 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude27,092 km
Orbital Velocity12,425 km/h
Velocity3.45 km/s
Orbital Period16 hours 56 minutes
Orbits / Day1.42
Eccentricity0.7975
Semi-Major Axis33,463 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2025-01-04
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
2025-001B
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 2025-01-04 from Cape Canaveral Space Force Station, United States on the Thuraya 4-NGS launch. As a relatively recent addition to the catalogue, its orbital elements are well-characterised. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 404 km and 53,780 km with an inclination of 24.2°. It travels at approximately 12,425 km/h (3.45 km/s), completing one full orbit every 16 hours 56 minutes — that’s roughly 1.42 orbits per day. Its orbital eccentricity of 0.7975 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 404 km (perigee) and 53,780 km (apogee). It spends most of its 16 hours 56 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. With an inclination of 24.2°, FALCON 9 R/B passes over latitudes between 24.2°N and 24.2°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. United States operates approximately 13,201 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 404 km (perigee) and 53,780 km (apogee). It spends most of its 16 hours 56 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 62484) 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 2025-01-04 from Cape Canaveral Space Force Station, United States, 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 62484) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 12,425 km/h (3.45 km/s), completing one revolution every 16 hours 56 minutes. Learn more about highly elliptical orbits.