Orbital elements of H-2A R/B
| Launched | 27 June 2025 |
| Flight ended | – |
| Launch site | Tanegashima Space Center, Japan |
| Owner | Japan |
| NORAD ID | 64695 |
| 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 04 10:19:27 | 98.0762 | 0.00920 | 0.7834 | 168.8780 | 191.4500 | 14.90439 | – |
| 2026 Mar 08 18:57 | 2026 Mar 04 10:19:27 | 98.0762 | 0.00920 | 0.7834 | 168.8780 | 191.4500 | 14.90439 | – |
| 2026 Mar 07 18:57 | 2026 Mar 04 10:19:27 | 98.0762 | 0.00920 | 0.7834 | 168.8780 | 191.4500 | 14.90439 | – |
| 2026 Mar 06 18:56 | 2026 Mar 04 10:19:27 | 98.0762 | 0.00920 | 0.7834 | 168.8780 | 191.4500 | 14.90439 | – |
| 2026 Mar 05 18:56 | 2026 Mar 04 10:19:27 | 98.0762 | 0.00920 | 0.7834 | 168.8780 | 191.4500 | 14.90439 | – |
| 2026 Mar 04 18:57 | 2026 Mar 04 10:19:27 | 98.0762 | 0.00920 | 0.7834 | 168.8780 | 191.4500 | 14.90439 | – |
| 2026 Mar 03 18:56 | 2026 Feb 26 14:08:31 | 98.0741 | 0.00915 | 0.3854 | 188.0112 | 191.4500 | 14.90439 | – |
| 2026 Mar 02 18:57 | 2026 Feb 26 14:08:31 | 98.0741 | 0.00915 | 0.3854 | 188.0112 | 191.4500 | 14.90439 | – |
| 2026 Mar 01 18:57 | 2026 Feb 26 14:08:31 | 98.0741 | 0.00915 | 0.3854 | 188.0112 | 191.4500 | 14.90439 | – |
| 2026 Feb 28 18:56 | 2026 Feb 26 14:08:31 | 98.0741 | 0.00915 | 0.3854 | 188.0112 | 191.4500 | 14.90439 | – |
| 2026 Feb 27 19:05 | 2026 Feb 26 14:08:31 | 98.0741 | 0.00915 | 0.3854 | 188.0112 | 191.4500 | 14.90439 | – |
| 2026 Feb 26 20:45 | 2026 Feb 26 14:08:31 | 98.0741 | 0.00915 | 0.3854 | 188.0112 | 191.4500 | 14.90439 | – |