Spacecraft information: GOSAT 2
| Launched | 28 October 2018 |
| Flight ended | – |
| Status | Operational |
| Category |
Active satellites
|
| Launch site | Tanegashima Space Center, Japan |
| Owner | Japan |
| NORAD ID | 43672 |
| COSPAR ID | 2018-084B |
| Alternative names |
IBUKI 1 |
| Observing |
Current orbital elements
| Inclination | 97.868° |
| Eccentricity | 0.00014 |
| RA ascending node | 7.994 hr |
| Argument perigee | 93.690° |
| Mean anomaly | 266.448° |
| Orbital period | 97.018 min |
| Epoch of osculation | 06 Jan 2026, 07:02 |
Derived Quantities
| Min Altitude | 622.0 km |
| Mean Altitude | 623.0 km |
| Peak Altitude | 624.0 km |
Launched alongside
H-2A DEB H-2A DEB H-2A DEB H-2A DEB KHALIFASAT TEN-KOH DIWATA-2B STARS-AO AUTCUBE 2 H-2A R/B H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEB H-2A DEBOrbital History
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