Showing default

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.

Loading next visibility...
Identifier
60542, 2024-149CC
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
QPS Labs
Mission
Operational Commercial Radar Imaging
Bus & Motor
QSAT, Unknown motor
Mass
~120 kg wet, ~100 kg dry
Launch date (UTC)
2024-08-16 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 22 hours ago

TLE from 22 hours ago
0 QPS-SAR-8 AMATERU-IV
1 60542U 24149CC  26276.46308983  .00002137  00000-0  15491-3 0  9997
2 60542  97.6584 354.7277 0004667 102.0432 258.1317 15.05006186116555
Epoch: 2026-10-03T11:06Z
TLE epoch observation values (Epoch: 2026-10-03T11:06:50.961Z)
Latitude
-0.00006°
Longitude
175.84504°
Altitude
555.216 km
Speed
7.584 km/s
True Right ascension
23h 38m 54s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
02:50:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
551.716 km
Perigee altitude
545.251 km
Semi-major axis
6,926.62 km
Eccentricity
0.00047
Inclination
97.6584°
RAAN
354.7277°
Arg. of periapsis
102.0432°
True anomaly
258.07937°
Mean anomaly
258.1317°
Eccentric anomaly
258.10553°
Mean motion
3.76497 °/min
Orbital period
95.62 mins
BSTAR
0.00015491
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|