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QPS-SAR-7 TSUKUYOMI-II

NORAD 59447 Payload LEO 2024-066F ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
536 km
Apogee
540 km
Inclination
45.6°
Period
95.4 min
Mean Motion
15.09493575 rev/day
TLE Epoch
2026-08-03 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude538 km
Orbital Velocity27,344 km/h
Velocity7.60 km/s
Orbital Period95 minutes
Orbits / Day15.09
Eccentricity0.0003
Semi-Major Axis6,909 km
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2024-04-07
Launch Site
Cape Canaveral, Florida
Int'l Designator
2024-066F
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
QPS-SAR-7 TSUKUYOMI-II is an active satellite operated by Japan, launched on 2024-04-07 from Cape Canaveral, Florida on the Bandwagon-1 launch. It orbits in Low Earth Orbit (LEO) at altitudes between 536 km and 540 km with an inclination of 45.6°. It travels at approximately 27,344 km/h (7.60 km/s), completing one full orbit every 95 minutes — that’s roughly 15.09 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~3–10 years. Orbital Radar tracks QPS-SAR-7 TSUKUYOMI-II in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
QPS-SAR-7 TSUKUYOMI-II orbits at an average altitude of 538 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of QPS-SAR-7 TSUKUYOMI-II’s average altitude, there are currently 2,510 active payloads and 319 tracked debris or rocket body fragments — notable neighbours include STARLINK-1184, STARLINK-1276, STARLINK-1451. This makes it one of the more crowded altitude bands, containing roughly 14.1% of all active satellites. With an inclination of 45.6°, QPS-SAR-7 TSUKUYOMI-II passes over latitudes between 45.6°N and 45.6°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 200 active satellites in total, of which 55 share a similar altitude band with QPS-SAR-7 TSUKUYOMI-II.
❓ Frequently Asked Questions
QPS-SAR-7 TSUKUYOMI-II orbits in Low Earth Orbit (LEO) at altitudes between 536 km (perigee) and 540 km (apogee), with an average altitude of approximately 538 km. It completes one orbit every 95 minutes, travelling at approximately 27,344 km/h (16,991 mph).
QPS-SAR-7 TSUKUYOMI-II is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 59447. You can track QPS-SAR-7 TSUKUYOMI-II in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
QPS-SAR-7 TSUKUYOMI-II was launched on 2024-04-07 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: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks QPS-SAR-7 TSUKUYOMI-II (NORAD ID 59447) 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.
QPS-SAR-7 TSUKUYOMI-II travels at approximately 27,344 km/h (16,991 mph) — roughly 7.60 km/s. It completes 15.09 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.