Orbital elements of AYAME-2 DEB
| Launched | 21 February 1980 |
| Flight ended | – |
| Launch site | Tanegashima Space Center, Japan |
| Owner | Japan |
| NORAD ID | 38684 |
| 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 |
| 2024 Jun 18 17:54 | 2024 Jun 07 20:32:58 | 9.7502 | 0.44693 | 2.6104 | 294.3328 | 25.8172 | 1.77278 | – |
| 2024 Jun 17 17:53 | 2024 Jun 07 20:32:58 | 9.7502 | 0.44693 | 2.6104 | 294.3328 | 25.8172 | 1.77278 | – |
| 2024 Jun 16 17:56 | 2024 Jun 07 20:32:58 | 9.7502 | 0.44693 | 2.6104 | 294.3328 | 25.8172 | 1.77278 | – |
| 2024 Jun 15 17:53 | 2024 Jun 07 20:32:58 | 9.7502 | 0.44693 | 2.6104 | 294.3328 | 25.8172 | 1.77278 | – |
| 2024 Jun 14 17:53 | 2024 Jun 07 20:32:58 | 9.7502 | 0.44693 | 2.6104 | 294.3328 | 25.8172 | 1.77278 | – |
| 2024 Jun 13 17:56 | 2024 Jun 07 20:32:58 | 9.7502 | 0.44693 | 2.6104 | 294.3328 | 25.8172 | 1.77278 | – |
| 2024 Jun 12 17:53 | 2024 Jun 07 20:32:58 | 9.7502 | 0.44693 | 2.6104 | 294.3328 | 25.8172 | 1.77278 | – |
| 2024 Jun 11 17:52 | 2024 Jun 07 20:32:58 | 9.7502 | 0.44693 | 2.6104 | 294.3328 | 25.8172 | 1.77278 | – |
| 2024 Jun 10 17:53 | 2024 Jun 07 20:32:58 | 9.7502 | 0.44693 | 2.6104 | 294.3328 | 25.8172 | 1.77278 | – |
| 2024 Jun 09 17:52 | 2024 Jun 07 20:32:58 | 9.7502 | 0.44693 | 2.6104 | 294.3328 | 25.8172 | 1.77278 | – |
| 2024 Jun 08 17:52 | 2024 Jun 02 18:43:19 | 9.7461 | 0.44705 | 2.6353 | 293.5697 | 25.8172 | 1.77278 | – |
| 2024 Jun 07 17:53 | 2024 Jun 02 18:43:19 | 9.7461 | 0.44705 | 2.6353 | 293.5697 | 25.8172 | 1.77278 | – |
| 2024 Jun 06 17:52 | 2024 Jun 02 18:43:19 | 9.7461 | 0.44705 | 2.6353 | 293.5697 | 25.8172 | 1.77278 | – |
| 2024 Jun 05 17:52 | 2024 Jun 02 18:43:19 | 9.7461 | 0.44705 | 2.6353 | 293.5697 | 25.8172 | 1.77278 | – |