Orbital elements of CE-SAT-IE
| Launched | 16 February 2024 |
| Flight ended | – |
| Launch site | Tanegashima Space Center, Japan |
| Owner | Japan |
| NORAD ID | 58987 |
| 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 Mar 09 18:56 | 2026 Mar 09 09:32:25 | 98.0096 | 0.00037 | 8.3511 | 56.2765 | 303.8792 | 14.68188 | – |
| 2026 Mar 08 18:57 | 2026 Mar 08 02:27:47 | 98.0099 | 0.00037 | 8.2666 | 59.0438 | 303.8792 | 14.68188 | – |
| 2026 Mar 07 18:57 | 2026 Mar 07 15:00:48 | 98.0099 | 0.00038 | 8.2354 | 60.3118 | 303.8792 | 14.68188 | – |
| 2026 Mar 06 18:56 | 2026 Mar 06 11:12:26 | 98.0102 | 0.00038 | 8.1598 | 62.7299 | 303.8792 | 14.68188 | – |
| 2026 Mar 05 18:56 | 2026 Mar 05 13:56:38 | 98.0104 | 0.00038 | 8.1020 | 64.7235 | 303.8792 | 14.68188 | – |
| 2026 Mar 04 18:57 | 2026 Mar 04 15:02:41 | 98.0106 | 0.00039 | 8.0397 | 66.8229 | 303.8792 | 14.68188 | – |
| 2026 Mar 03 18:56 | 2026 Mar 03 03:03:36 | 98.0110 | 0.00039 | 7.9418 | 70.0794 | 303.8792 | 14.68188 | – |
| 2026 Mar 02 18:57 | 2026 Mar 02 15:36:38 | 98.0112 | 0.00039 | 7.9107 | 71.1311 | 303.8792 | 14.68188 | – |
| 2026 Mar 01 18:57 | 2026 Mar 01 03:37:33 | 98.0115 | 0.00040 | 7.8128 | 74.3567 | 303.8792 | 14.68188 | – |
| 2026 Feb 28 18:56 | 2026 Feb 28 09:38:01 | 98.0120 | 0.00040 | 7.7639 | 76.0423 | 303.8792 | 14.68188 | – |
| 2026 Feb 27 19:05 | 2026 Feb 27 02:33:21 | 98.0123 | 0.00040 | 7.6793 | 78.7398 | 303.8792 | 14.68188 | – |
| 2026 Feb 26 20:45 | 2026 Feb 26 15:06:23 | 98.0125 | 0.00041 | 7.6482 | 79.7569 | 303.8792 | 14.68188 | – |