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H-2A R/B

NORAD 49337 Rocket Body MEO 2021-096B
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Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
211 km
Apogee
28251 km
Inclination
31.6°
Period
490.7 min
Mean Motion
2.93435614 rev/day
TLE Epoch
2026-06-24 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude14,231 km
Orbital Velocity15,835 km/h
Velocity4.40 km/s
Orbital Period8 hours 11 minutes
Orbits / Day2.93
Eccentricity0.6805
Semi-Major Axis20,602 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2021-10-26
Launch Site
TNSTA
Int'l Designator
2021-096B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
H-2A R/B is a spent rocket body associated with Japan, launched on 2021-10-26 from TNSTA on the QZSS 1R launch. It orbits in Medium Earth Orbit (MEO) at altitudes between 211 km and 28,251 km with an inclination of 31.6°. It travels at approximately 15,835 km/h (4.40 km/s), completing one full orbit every 8 hours 11 minutes — that’s roughly 2.93 orbits per day. Its orbital eccentricity of 0.6805 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Spent rocket bodies like H-2A 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
H-2A R/B orbits at an average altitude of 14,231 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 H-2A 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 31.6°, H-2A R/B passes over latitudes between 31.6°N and 31.6°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. Japan operates approximately 190 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
H-2A R/B orbits in Medium Earth Orbit (MEO) at altitudes between 211 km (perigee) and 28,251 km (apogee), with an average altitude of approximately 14,231 km. It completes one orbit every 8 hours 11 minutes, travelling at approximately 15,835 km/h (9,839 mph).
H-2A R/B (NORAD ID 49337) is a spent rocket body — the upper stage of a launch vehicle attributed to Japan. 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.
H-2A R/B was launched on 2021-10-26 from TNSTA. 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 H-2A R/B (NORAD ID 49337) 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.
H-2A R/B travels at approximately 15,835 km/h (9,839 mph) — roughly 4.40 km/s. It completes 2.93 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 6 sunrises and sunsets every 24 hours.