FALCON 9 R/B
NORAD 42819
Rocket Body
MEO
2017-041B
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MEO · NORAD 42819
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
198 km
Apogee
38752 km
Inclination
25.1°
Period
689.5 min
Mean Motion
2.09009218 rev/day
TLE Epoch
2026-07-16 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,475 km
Orbital Velocity14,138 km/h
Velocity3.93 km/s
Orbital Period11 hours 29 minutes
Orbits / Day2.09
Eccentricity0.7458
Semi-Major Axis25,846 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2017-07-05
Launch Site
Cape Canaveral, Florida
Int'l Designator
2017-041B
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 2017-07-05 from Cape Canaveral, Florida on the Intelsat IS-35e launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 198 km and 38,752 km with an inclination of 25.1°. It travels at approximately 14,138 km/h (3.93 km/s), completing one full orbit every 11 hours 29 minutes — that’s roughly 2.09 orbits per day. Its orbital eccentricity of 0.7458 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 orbits at an average altitude of 19,475 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. With an inclination of 25.1°, FALCON 9 R/B passes over latitudes between 25.1°N and 25.1°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 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 198 km (perigee) and 38,752 km (apogee), with an average altitude of approximately 19,475 km. It completes one orbit every 11 hours 29 minutes, travelling at approximately 14,138 km/h (8,785 mph).
FALCON 9 R/B (NORAD ID 42819) 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 2017-07-05 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 42819) 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 14,138 km/h (8,785 mph) — roughly 3.93 km/s. It completes 2.09 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.