Spacecraft information: AUTCUBE 2
| Launched | 28 October 2018 |
| Flight ended | – |
| Status | Operational |
| Category |
Active satellites
|
| Launch site | Tanegashima Space Center, Japan |
| Owner | Japan |
| NORAD ID | 43681 |
| COSPAR ID | 2018-084K |
| Observing |
Current orbital elements
| Inclination | 98.079° |
| Eccentricity | 0.00083 |
| RA ascending node | 12.169 hr |
| Argument perigee | 305.380° |
| Mean anomaly | 54.666° |
| Orbital period | 95.469 min |
| Epoch of osculation | 16 Dec 2025, 23:35 |
Derived Quantities
| Min Altitude | 542.7 km |
| Mean Altitude | 548.4 km |
| Peak Altitude | 554.1 km |
Launched alongside
H-2A DEB GOSAT 2 H-2A DEB H-2A DEB H-2A DEB KHALIFASAT TEN-KOH DIWATA-2B STARS-AO 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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