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QPS-SAR-5 TSUKUYOMI-I

NORAD 58578 Payload LEO 2023-196A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
479 km
Apogee
517 km
Inclination
42.0°
Period
94.6 min
Mean Motion
15.22620281 rev/day
TLE Epoch
2026-06-19 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude498 km
Orbital Velocity27,424 km/h
Velocity7.62 km/s
Orbital Period95 minutes
Orbits / Day15.23
Eccentricity0.0028
Semi-Major Axis6,869 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2023-12-15
Launch Site
RLLC
Int'l Designator
2023-196A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
QPS-SAR-5 TSUKUYOMI-I is an active satellite operated by Japan, launched on 2023-12-15 from RLLC. It orbits in Low Earth Orbit (LEO) at altitudes between 479 km and 517 km with an inclination of 42.0°. It travels at approximately 27,424 km/h (7.62 km/s), completing one full orbit every 95 minutes — that’s roughly 15.23 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Orbital Radar tracks QPS-SAR-5 TSUKUYOMI-I 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-5 TSUKUYOMI-I orbits at an average altitude of 498 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-5 TSUKUYOMI-I’s average altitude, there are currently 9,150 active payloads and 241 tracked debris or rocket body fragments — notable neighbours include STARLINK-1017, STARLINK-1039, STARLINK-1047. This makes it one of the more crowded altitude bands, containing roughly 52.5% of all active satellites. With an inclination of 42.0°, QPS-SAR-5 TSUKUYOMI-I passes over latitudes between 42.0°N and 42.0°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 189 active satellites in total, of which 31 share a similar altitude band with QPS-SAR-5 TSUKUYOMI-I.
❓ Frequently Asked Questions
QPS-SAR-5 TSUKUYOMI-I orbits in Low Earth Orbit (LEO) at altitudes between 479 km (perigee) and 517 km (apogee), with an average altitude of approximately 498 km. It completes one orbit every 95 minutes, travelling at approximately 27,424 km/h (17,040 mph).
QPS-SAR-5 TSUKUYOMI-I is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 58578. You can track QPS-SAR-5 TSUKUYOMI-I in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
QPS-SAR-5 TSUKUYOMI-I was launched on 2023-12-15 from RLLC. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks QPS-SAR-5 TSUKUYOMI-I (NORAD ID 58578) 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-5 TSUKUYOMI-I travels at approximately 27,424 km/h (17,040 mph) — roughly 7.62 km/s. It completes 15.23 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.