Orbital elements of H-2A DEB
| Launched | 3 February 2002 |
| Flight ended | – |
| Launch site | Tanegashima Space Center, Japan |
| Owner | Japan |
| NORAD ID | 28237 |
| 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 |
| 2025 Nov 02 18:57 | 2025 Oct 03 00:33:15 | 28.6537 | 0.70795 | 18.4354 | 268.6001 | 16.6909 | 2.46361 | 6.243 |
| 2025 Nov 01 18:58 | 2025 Oct 03 00:33:15 | 28.6537 | 0.70795 | 18.4354 | 268.6001 | 16.6909 | 2.46361 | 6.243 |
| 2025 Oct 31 18:57 | 2025 Oct 03 00:33:15 | 28.6537 | 0.70795 | 18.4354 | 268.6001 | 16.6909 | 2.46361 | 6.243 |
| 2025 Oct 30 18:57 | 2025 Oct 03 00:33:15 | 28.6537 | 0.70795 | 18.4354 | 268.6001 | 16.6909 | 2.46361 | 6.243 |
| 2025 Oct 29 18:57 | 2025 Oct 03 00:33:15 | 28.6537 | 0.70795 | 18.4354 | 268.6001 | 16.6909 | 2.46361 | 6.243 |
| 2025 Oct 17 17:56 | 2025 Oct 03 00:33:06 | 28.6537 | 0.70787 | 18.4356 | 268.5974 | 16.6909 | 2.46361 | 6.243 |
| 2025 Oct 16 17:56 | 2025 Oct 03 00:33:06 | 28.6537 | 0.70787 | 18.4356 | 268.5974 | 16.6909 | 2.46361 | 6.243 |
| 2025 Oct 15 17:56 | 2025 Oct 03 00:33:06 | 28.6537 | 0.70787 | 18.4356 | 268.5974 | 16.6909 | 2.46361 | 6.243 |
| 2025 Oct 14 17:56 | 2025 Oct 03 00:33:06 | 28.6537 | 0.70787 | 18.4356 | 268.5974 | 16.6909 | 2.46361 | 6.243 |
| 2025 Oct 12 17:56 | 2025 Oct 03 00:33:06 | 28.6537 | 0.70787 | 18.4356 | 268.5974 | 16.6909 | 2.46361 | 6.243 |
| 2025 Oct 11 17:57 | 2025 Oct 03 00:33:06 | 28.6537 | 0.70787 | 18.4356 | 268.5974 | 16.6909 | 2.46361 | 6.243 |
| 2025 Oct 09 17:56 | 2025 Oct 03 00:33:06 | 28.6537 | 0.70787 | 18.4356 | 268.5974 | 16.6909 | 2.46361 | 6.243 |
| 2025 Oct 08 17:56 | 2025 Oct 03 00:33:06 | 28.6537 | 0.70787 | 18.4356 | 268.5974 | 16.6909 | 2.46361 | 6.243 |
| 2025 Oct 07 17:56 | 2025 Oct 03 00:33:06 | 28.6537 | 0.70787 | 18.4356 | 268.5974 | 16.6909 | 2.46361 | 6.243 |