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FALCON HEAVY R/B

NORAD 68894 Rocket Body MEO 2026-096B
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
22944 km
Apogee
33151 km
Inclination
2.6°
Period
1059.5 min
Mean Motion
1.35919154 rev/day
TLE Epoch
2026-06-26 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude28,048 km
Orbital Velocity12,251 km/h
Velocity3.40 km/s
Orbital Period17 hours 39 minutes
Orbits / Day1.36
Eccentricity0.1483
Semi-Major Axis34,419 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
2026-04-29
Launch Site
Cape Canaveral, Florida
Int'l Designator
2026-096B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
FALCON HEAVY R/B is a spent rocket body associated with United States, launched on 2026-04-29 from Cape Canaveral, Florida on the Viasat 3F3 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 22,944 km and 33,151 km with an inclination of 2.6°. It travels at approximately 12,251 km/h (3.40 km/s), completing one full orbit every 17 hours 39 minutes — that’s roughly 1.36 orbits per day. Its orbital eccentricity of 0.1483 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like FALCON HEAVY 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 HEAVY R/B orbits at an average altitude of 28,048 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 2.6°, FALCON HEAVY R/B passes over latitudes between 2.6°N and 2.6°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 HEAVY R/B orbits in Medium Earth Orbit (MEO) at altitudes between 22,944 km (perigee) and 33,151 km (apogee), with an average altitude of approximately 28,048 km. It completes one orbit every 17 hours 39 minutes, travelling at approximately 12,251 km/h (7,612 mph).
FALCON HEAVY R/B (NORAD ID 68894) 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 HEAVY R/B was launched on 2026-04-29 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 HEAVY R/B (NORAD ID 68894) 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 HEAVY R/B travels at approximately 12,251 km/h (7,612 mph) — roughly 3.40 km/s. It completes 1.36 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 3 sunrises and sunsets every 24 hours.