Showing default

QPS-SAR-9 SUSANOO-I, 63205

Orbit data source: Space-Track

QPS-SAR-9 SUSANOO-I, 63205 is a payload satellite owned by QPS Labs (JP) in LEO that was launched on Sat, 15 Mar 2025 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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
63205, 2025-050A
Orbit
LEO
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)
2025-03-15 (8 months ago)
Launch vehicle
ELECTRON
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Hex Cyl + 2 Pan + 1 Dish, 14.5 m
Radar Cross Section
1.179 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 4 hours ago

TLE from 4 hours ago
0 QPS-SAR-9 SUSANOO-I
1 63205U 25050A   25311.85412575  .00009983  00000-0  80115-3 0  9994
2 63205  42.0204 242.7780 0000208  98.7895 261.2954 15.00091026 35681
Epoch: 2025-11-07T20:29Z
TLE epoch observation values (Epoch: 2025-11-07T20:29:56.464Z)
Latitude
-0.00006°
Longitude
-111.99945°
Altitude
566.308 km
Speed
7.58 km/s
True Right ascension
16h 11m 06s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
21:08:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.844 km
Perigee altitude
568.555 km
Semi-major axis
6,946.836 km
Eccentricity
0.00002
Inclination
42.0204°
RAAN
242.778°
Arg. of periapsis
98.7895°
True anomaly
261.29304°
Mean anomaly
261.2954°
Eccentric anomaly
261.29422°
Mean motion
3.74854 °/min
Orbital period
96.04 mins
BSTAR
0.00080115
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...
Other satellites on launch #50 in the year 2025 (2025-03-15 UTC)

Documentation

Showing up to 5 results
|