Orbital elements of AYAME-2 DEB
| Launched | 21 February 1980 |
| Flight ended | – |
| Launch site | Tanegashima Space Center, Japan |
| Owner | Japan |
| NORAD ID | 28999 |
| 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 Feb 05 18:58 | 2026 Feb 01 10:00:06 | 9.2051 | 0.43827 | 2.9720 | 283.2012 | 32.6162 | 1.75836 | – |
| 2026 Feb 04 18:57 | 2026 Feb 01 10:00:06 | 9.2051 | 0.43827 | 2.9720 | 283.2012 | 32.6162 | 1.75836 | – |
| 2026 Feb 03 18:56 | 2026 Feb 01 10:00:06 | 9.2051 | 0.43827 | 2.9720 | 283.2012 | 32.6162 | 1.75836 | – |
| 2026 Feb 02 18:56 | 2026 Feb 01 10:00:06 | 9.2051 | 0.43827 | 2.9720 | 283.2012 | 32.6162 | 1.75836 | – |
| 2026 Feb 01 18:56 | 2026 Jan 27 07:10:32 | 9.1993 | 0.43819 | 2.9949 | 282.4348 | 32.6162 | 1.75836 | – |
| 2026 Jan 31 18:56 | 2026 Jan 27 07:10:32 | 9.1993 | 0.43819 | 2.9949 | 282.4348 | 32.6162 | 1.75836 | – |
| 2026 Jan 30 18:57 | 2026 Jan 27 07:10:32 | 9.1993 | 0.43819 | 2.9949 | 282.4348 | 32.6162 | 1.75836 | – |
| 2026 Jan 29 18:56 | 2026 Jan 27 07:10:32 | 9.1993 | 0.43819 | 2.9949 | 282.4348 | 32.6162 | 1.75836 | – |
| 2026 Jan 28 18:56 | 2026 Jan 27 07:10:32 | 9.1993 | 0.43819 | 2.9949 | 282.4348 | 32.6162 | 1.75836 | – |
| 2026 Jan 27 18:56 | 2026 Jan 21 14:42:07 | 9.1942 | 0.43814 | 3.0210 | 281.5766 | 32.6162 | 1.75836 | – |
| 2026 Jan 26 18:57 | 2026 Jan 21 14:42:07 | 9.1942 | 0.43814 | 3.0210 | 281.5766 | 32.6162 | 1.75836 | – |
| 2026 Jan 25 18:57 | 2026 Jan 21 14:42:07 | 9.1942 | 0.43814 | 3.0210 | 281.5766 | 32.6162 | 1.75836 | – |
| 2026 Jan 24 18:58 | 2026 Jan 21 14:42:07 | 9.1942 | 0.43814 | 3.0210 | 281.5766 | 32.6162 | 1.75836 | – |