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QPS-SAR-7 TSUKUYOMI-II, 59447

Orbit data source: Space-Track

QPS-SAR-7 TSUKUYOMI-II, 59447 is a payload satellite owned by QPS Labs (JP) in LEO that was launched on Sun, 07 Apr 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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Identifier
59447, 2024-066F
Orbit
LEO
Country
Flag of JPJP / JPN
Related business
Manufacturer
QPS Labs
Mission
Operational spacecraft
Bus & Motor
QSAT, Unknown motor
Mass
~120 kg wet, ~100 kg dry
Launch date (UTC)
2024-04-07 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 QPS-SAR-7 TSUKUYOMI-II
1 59447U 24066F   25247.63108553  .00008990  00000-0  66364-3 0  9992
2 59447  45.6064 298.4353 0003631 299.0298  61.0221 15.03638388 77160
Epoch: 2025-09-04T15:08Z
TLE epoch observation values (Epoch: 2025-09-04T15:08:45.789Z)
Latitude
-0.00003°
Longitude
87.25363°
Altitude
554.535 km
Speed
7.587 km/s
True Right ascension
19h 53m 44s
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
23:41:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
559.698 km
Perigee altitude
554.662 km
Semi-major axis
6,935.317 km
Eccentricity
0.00036
Inclination
45.6064°
RAAN
298.4353°
Arg. of periapsis
299.0298°
True anomaly
61.05851°
Mean anomaly
61.0221°
Eccentric anomaly
61.0403°
Mean motion
3.75789 °/min
Orbital period
95.8 mins
BSTAR
0.00066364
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Documentation

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