Orbital elements of H-2A R/B
| Launched | 1 November 2016 |
| Flight ended | – |
| Launch site | Tanegashima Space Center, Japan |
| Owner | Japan |
| NORAD ID | 41837 |
| Date fetched |
Epoch osculation |
Inc. [°] |
Ecc. | RA asc node [hr] |
Arg Peri. [°] |
Mean anom [°] |
Mean motion [rev/day] |
Abs. mag |
| Date fetched |
Epoch osculation |
Inc. [°] |
Ecc. | RA asc node [hr] |
Arg Peri. [°] |
Mean anom [°] |
Mean motion [rev/day] |
Abs. mag |
| 2026 Mar 09 18:56 | 2026 Mar 03 21:09:46 | 22.5761 | 0.63818 | 19.5525 | 263.6509 | 25.2339 | 3.52842 | – |
| 2026 Mar 08 18:57 | 2026 Mar 03 21:09:46 | 22.5761 | 0.63818 | 19.5525 | 263.6509 | 25.2339 | 3.52842 | – |
| 2026 Mar 07 18:57 | 2026 Mar 03 21:09:46 | 22.5761 | 0.63818 | 19.5525 | 263.6509 | 25.2339 | 3.52842 | – |
| 2026 Mar 06 18:56 | 2026 Mar 03 21:09:46 | 22.5761 | 0.63818 | 19.5525 | 263.6509 | 25.2339 | 3.52842 | – |
| 2026 Mar 05 18:56 | 2026 Mar 03 21:09:46 | 22.5761 | 0.63818 | 19.5525 | 263.6509 | 25.2339 | 3.52842 | – |
| 2026 Mar 04 18:57 | 2026 Mar 03 21:09:46 | 22.5761 | 0.63818 | 19.5525 | 263.6509 | 25.2339 | 3.52842 | – |
| 2026 Mar 03 18:56 | 2026 Feb 25 22:21:28 | 22.5485 | 0.63808 | 19.8170 | 256.6021 | 25.2339 | 3.52842 | – |
| 2026 Mar 02 18:57 | 2026 Feb 25 22:21:28 | 22.5485 | 0.63808 | 19.8170 | 256.6021 | 25.2339 | 3.52842 | – |
| 2026 Mar 01 18:57 | 2026 Feb 25 22:21:28 | 22.5485 | 0.63808 | 19.8170 | 256.6021 | 25.2339 | 3.52842 | – |
| 2026 Feb 28 18:56 | 2026 Feb 25 22:21:28 | 22.5485 | 0.63808 | 19.8170 | 256.6021 | 25.2339 | 3.52842 | – |
| 2026 Feb 27 19:05 | 2026 Feb 25 22:21:28 | 22.5485 | 0.63808 | 19.8170 | 256.6021 | 25.2339 | 3.52842 | – |
| 2026 Feb 26 20:45 | 2026 Feb 25 22:21:28 | 22.5485 | 0.63808 | 19.8170 | 256.6021 | 25.2339 | 3.52842 | – |