QPS-SAR-1 IZANAGI, 44856 (Decayed)

Orbit data source: Space-Track

QPS-SAR-1 IZANAGI, 44856 was a payload satellite owned by QPS Labs (JP) in LEO that was launched on Wed, 11 Dec 2019 UTC via a PSLV-QL launch vehicle from the Sirharikota (SRI). Payloads include a variety of satellites, spacecraft, and rockets 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.

Not visible in the next 10 days

QPS-SAR-1 IZANAGI details

Identifier	44856, 2019-089E
Orbit	Decayed
Last TLE update	3 months ago
Origin	QPS Labs (JP / JPN)
Manufacturer	QPS Labs
Mission	Decayed Commercial Radar Imaging
Bus & Motor	QSAT, Unknown motor
Mass	~120 kg wet, ~100 kg dry
Launch date (UTC)	2019-12-11 (5 years ago)
Launch vehicle	PSLV-QL
Launch site	Sirharikota (SRI)
Object type	Payload Rocket body Debris
Shape & HBR	Hex Cyl + 2 Pan + 1 Dish, Unknown HBR
Radar Cross Section	1.179 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 3 months ago

0 QPS-SAR-1 IZANAGI
1 44856U 19089E   24276.76840433  .15578814  37316-5  26260-2 0  9992
2 44856  36.9296  36.2523 0007425 357.0003 127.4349 16.31997839265459

Epoch: 2024-10-02T18:26Z

Definitive object data (Epoch: 2024-10-02T18:26:30.134Z)

Latitude	29.8079°
Longitude	-121.60873°
Altitude	189.945 km
Speed	7.796 km/s
True Right ascension	11h 07m 55s
True Declination	29° 38' 49"
Sunlit	Object was in daylight at TLE epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude	195.134 km
Perigee altitude	185.38 km
Semi-major axis	6,568.394 km
Eccentricity	0.0007425
Inclination	36.9296°
RAAN	36.2523°
Arg. of periapsis	357.0003°
True anomaly	127.50242°
Mean anomaly	127.4349°
Eccentric anomaly	127.46867°
Mean motion	4.07713 °/min
BSTAR	0.002626
Orbital period	88.3 mins