QPS-SAR-8 AMATERU-IV, 60542
Orbit data source: Space-Track
QPS-SAR-8 AMATERU-IV, 60542 is a payload satellite owned by QPS Labs (JP) in SSO that was launched on Fri, 16 Aug 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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60542 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
QPS Labs
Mission
Operational Commercial Radar Imaging
Bus & Motor
QSAT, Unknown motor
Mass
~120 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Cyl + 2 Pan + 1 Dish, 1.8 m
Radar Cross Section
1.179 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 QPS-SAR-8 AMATERU-IV
1 60542U 24149CC 26080.48710421 .00007357 00000-0 54831-3 0 9996
2 60542 97.6709 160.4241 0004337 66.6362 293.5319 15.03184016 87096Epoch: 2026-03-21T11:41Z
TLE epoch observation values (Epoch: 2026-03-21T11:41:25.803Z)
Latitude
-0.00005°
Longitude
166.05948°
Altitude
558.945 km
Speed
7.583 km/s
True Right ascension
10h 41m 41s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
05:48:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
557.092 km
Perigee altitude
551.079 km
Semi-major axis
6,932.222 km
Eccentricity
0.00043
Inclination
97.6709°
RAAN
160.4241°
Arg. of periapsis
66.6362°
True anomaly
293.48632°
Mean anomaly
293.5319°
Eccentric anomaly
293.50911°
Mean motion
3.7604 °/min
Orbital period
95.73 mins
BSTAR
0.00054831
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.QPS-SAR-8 AMATERU-IV Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-22 05:23:24.506Z | 173.268° S | 2026-03-22 05:26:24.506Z | 243.932° WSW | 44.047° | 2026-03-22 05:30:24.506Z | 344.422° N |
| 5 mins | 2026-03-22 18:37:24.506Z | 343.678° N | 2026-03-22 18:39:24.506Z | 289.286° WNW | 32.913° | 2026-03-22 18:42:24.506Z | 222.041° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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