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 Nov 21 18:53 | 2024 Nov 10 12:38:54 | 9.8389 | 0.44791 | 1.8542 | 317.0984 | 15.6450 | 1.77292 | – |
2024 Nov 20 18:53 | 2024 Nov 10 12:38:54 | 9.8389 | 0.44791 | 1.8542 | 317.0984 | 15.6450 | 1.77292 | – |
2024 Nov 02 18:53 | 2024 Oct 22 21:58:02 | 9.8337 | 0.44723 | 1.9435 | 314.3885 | 15.6450 | 1.77292 | – |
2024 Nov 01 18:53 | 2024 Oct 22 21:58:02 | 9.8337 | 0.44723 | 1.9435 | 314.3885 | 15.6450 | 1.77292 | – |
2024 Oct 31 18:53 | 2024 Oct 22 21:58:02 | 9.8337 | 0.44723 | 1.9435 | 314.3885 | 15.6450 | 1.77292 | – |
2024 Oct 30 18:53 | 2024 Oct 22 21:58:02 | 9.8337 | 0.44723 | 1.9435 | 314.3885 | 15.6450 | 1.77292 | – |
2024 Oct 29 18:53 | 2024 Oct 22 21:58:02 | 9.8337 | 0.44723 | 1.9435 | 314.3885 | 15.6450 | 1.77292 | – |
2024 Oct 28 18:53 | 2024 Oct 22 21:58:02 | 9.8337 | 0.44723 | 1.9435 | 314.3885 | 15.6450 | 1.77292 | – |
2024 Oct 27 18:55 | 2024 Oct 22 21:58:02 | 9.8337 | 0.44723 | 1.9435 | 314.3885 | 15.6450 | 1.77292 | – |
2024 Oct 26 17:53 | 2024 Oct 22 21:58:02 | 9.8337 | 0.44723 | 1.9435 | 314.3885 | 15.6450 | 1.77292 | – |
2024 Oct 25 17:53 | 2024 Oct 22 21:58:02 | 9.8337 | 0.44723 | 1.9435 | 314.3885 | 15.6450 | 1.77292 | – |