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H-2A R/B
Launch Details
| Launched | 16 February 2016 |
| Flight ended | – |
| Status | Unknown |
| Launch site | Tanegashima Space Center, Japan |
| Owner | Japan |
| NORAD ID | 41341 |
| COSPAR ID | 2016-012E |
| Observing |
Current orbital elements
| Inclination | 30.626° |
| Eccentricity | 0.00059 |
| RA ascending node | 3.888 hr |
| Argument perigee | 291.924° |
| Mean anomaly | 68.076° |
| Orbital period | 93.431 min |
| Epoch of osculation | 29 Oct 2025, 12:13 |
Derived Quantities
| Min Altitude | 445.5 km |
| Mean Altitude | 449.6 km |
| Peak Altitude | 453.6 km |
Orbital History
Drag the graphs below left or right to change the time range, or use your scroll wheel to zoom in or out.
Launched alongside
ASTRO-H CHUBUSAT-2 CHUBUSAT-3 HORYU-4 H-2A DEB ASTRO-H ASTRO-H ASTRO-H ASTRO-H ASTRO-H ASTRO-H ASTRO-H ASTRO-H ASTRO-H ASTRO-H ASTRO-H DEB ASTRO-H DEB H-2A DEB