Orbital elements of AYAME-2 DEB
| Launched | 21 February 1980 |
| Flight ended | – |
| Launch site | Tanegashima Space Center, Japan |
| Owner | Japan |
| NORAD ID | 38685 |
| 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 Jan 29 03:45:11 | 10.0284 | 0.44429 | 1.9222 | 312.8383 | 17.3191 | 1.76321 | – |
| 2026 Feb 04 18:57 | 2026 Jan 29 03:45:11 | 10.0284 | 0.44429 | 1.9222 | 312.8383 | 17.3191 | 1.76321 | – |
| 2026 Feb 03 18:56 | 2026 Jan 29 03:45:11 | 10.0284 | 0.44429 | 1.9222 | 312.8383 | 17.3191 | 1.76321 | – |
| 2026 Feb 02 18:56 | 2026 Jan 29 03:45:11 | 10.0284 | 0.44429 | 1.9222 | 312.8383 | 17.3191 | 1.76321 | – |
| 2026 Feb 01 18:56 | 2026 Jan 27 10:55:22 | 10.0270 | 0.44419 | 1.9305 | 312.5795 | 17.3191 | 1.76321 | – |
| 2026 Jan 31 18:56 | 2026 Jan 27 10:55:22 | 10.0270 | 0.44419 | 1.9305 | 312.5795 | 17.3191 | 1.76321 | – |
| 2026 Jan 30 18:57 | 2026 Jan 27 10:55:22 | 10.0270 | 0.44419 | 1.9305 | 312.5795 | 17.3191 | 1.76321 | – |
| 2026 Jan 29 18:56 | 2026 Jan 27 10:55:22 | 10.0270 | 0.44419 | 1.9305 | 312.5795 | 17.3191 | 1.76321 | – |
| 2026 Jan 28 18:56 | 2026 Jan 27 10:55:22 | 10.0270 | 0.44419 | 1.9305 | 312.5795 | 17.3191 | 1.76321 | – |
| 2026 Jan 27 18:56 | 2026 Jan 21 18:49:21 | 10.0240 | 0.44408 | 1.9575 | 311.7155 | 17.3191 | 1.76321 | – |
| 2026 Jan 26 18:57 | 2026 Jan 21 18:49:21 | 10.0240 | 0.44408 | 1.9575 | 311.7155 | 17.3191 | 1.76321 | – |
| 2026 Jan 25 18:57 | 2026 Jan 21 18:49:21 | 10.0240 | 0.44408 | 1.9575 | 311.7155 | 17.3191 | 1.76321 | – |
| 2026 Jan 24 18:58 | 2026 Jan 21 18:49:21 | 10.0240 | 0.44408 | 1.9575 | 311.7155 | 17.3191 | 1.76321 | – |