H-1 R/B
NORAD 20491
Rocket Body
LEO
1990-013D
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LEO · NORAD 20491
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Altitude (km)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
890 km
Apogee
1605 km
Inclination
99.1°
Period
110.5 min
Mean Motion
13.03735053 rev/day
TLE Epoch
2026-06-25 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,248 km
Orbital Velocity26,040 km/h
Velocity7.23 km/s
Orbital Period110 minutes
Orbits / Day13.04
Eccentricity0.0469
Semi-Major Axis7,619 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
1990-02-07
Launch Site
TNSTA
Int'l Designator
1990-013D
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
H-1 R/B is a spent rocket body associated with Japan, launched on 1990-02-07 from TNSTA on the Mos-1b launch. With over 36 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 890 km and 1,605 km with an inclination of 99.1°. It travels at approximately 26,040 km/h (7.23 km/s), completing one full orbit every 110 minutes — that’s roughly 13.04 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Spent rocket bodies like H-1 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-1 R/B orbits at an average altitude of 1,248 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of H-1 R/B’s average altitude, there are currently 359 active payloads and 304 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0008, ONEWEB-0007, ONEWEB-0006. With an inclination of 99.1°, H-1 R/B passes over latitudes between 99.1°N and 99.1°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. 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-1 R/B orbits in Low Earth Orbit (LEO) at altitudes between 890 km (perigee) and 1,605 km (apogee), with an average altitude of approximately 1,248 km. It completes one orbit every 110 minutes, travelling at approximately 26,040 km/h (16,180 mph).
H-1 R/B (NORAD ID 20491) 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-1 R/B was launched on 1990-02-07 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks H-1 R/B (NORAD ID 20491) 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-1 R/B travels at approximately 26,040 km/h (16,180 mph) — roughly 7.23 km/s. It completes 13.04 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 sunrises and sunsets every 24 hours.