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 Dec 25 18:57 | 2025 Dec 20 06:57:34 | 28.5895 | 0.70568 | 16.4080 | 317.9838 | 5.7614 | 2.46666 | 6.243 |
| 2025 Dec 24 18:56 | 2025 Dec 20 06:57:34 | 28.5895 | 0.70568 | 16.4080 | 317.9838 | 5.7614 | 2.46666 | 6.243 |
| 2025 Dec 23 18:56 | 2025 Dec 20 06:57:34 | 28.5895 | 0.70568 | 16.4080 | 317.9838 | 5.7614 | 2.46666 | 6.243 |
| 2025 Dec 22 18:57 | 2025 Dec 20 06:57:34 | 28.5895 | 0.70568 | 16.4080 | 317.9838 | 5.7614 | 2.46666 | 6.243 |
| 2025 Dec 21 18:57 | 2025 Dec 20 06:57:34 | 28.5895 | 0.70568 | 16.4080 | 317.9838 | 5.7614 | 2.46666 | 6.243 |
| 2025 Dec 20 18:57 | 2025 Dec 20 06:57:34 | 28.5895 | 0.70568 | 16.4080 | 317.9838 | 5.7614 | 2.46666 | 6.243 |