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H-2A R/B

NORAD 41037 Rocket Body MEO 2015-068B
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
2677 km
Apogee
35668 km
Inclination
19.4°
Period
677.4 min
Mean Motion
2.12565874 rev/day
TLE Epoch
2026-06-25 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude19,173 km
Orbital Velocity14,221 km/h
Velocity3.95 km/s
Orbital Period11 hours 17 minutes
Orbits / Day2.13
Eccentricity0.6458
Semi-Major Axis25,544 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2015-11-24
Launch Site
TNSTA
Int'l Designator
2015-068B
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 2015-11-24 from TNSTA on the Telstar 12V launch. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Medium Earth Orbit (MEO) at altitudes between 2,677 km and 35,668 km with an inclination of 19.4°. It travels at approximately 14,221 km/h (3.95 km/s), completing one full orbit every 11 hours 17 minutes — that’s roughly 2.13 orbits per day. Its orbital eccentricity of 0.6458 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 19,173 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 140 active payloads and 13 tracked debris or rocket body fragments — notable neighbours include COSMOS 1414 (GLONASS), COSMOS 1490 (GLONASS), COSMOS 1492 (GLONASS). With an inclination of 19.4°, H-2A R/B passes over latitudes between 19.4°N and 19.4°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. 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 2,677 km (perigee) and 35,668 km (apogee), with an average altitude of approximately 19,173 km. It completes one orbit every 11 hours 17 minutes, travelling at approximately 14,221 km/h (8,837 mph).
H-2A R/B (NORAD ID 41037) 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 2015-11-24 from TNSTA. View the full satellite launch log.
Yes — Orbital Radar tracks H-2A R/B (NORAD ID 41037) 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 14,221 km/h (8,837 mph) — roughly 3.95 km/s. It completes 2.13 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.