Orbital elements of JCSAT-5A
| Launched | 11 April 2006 |
| Flight ended | – |
| Launch site | Sea Launch Platform (mobile) |
| Owner | Japan |
| NORAD ID | 29045 |
| 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 11 18:56 | 2026 Mar 11 12:29:33 | 0.8548 | 0.00021 | 5.6990 | 328.4240 | 74.7109 | 1.00271 | – |
| 2026 Mar 10 18:56 | 2026 Mar 10 12:43:05 | 0.8524 | 0.00020 | 5.7002 | 326.9762 | 74.7109 | 1.00271 | – |
| 2026 Mar 09 18:56 | 2026 Mar 09 11:02:43 | 0.8499 | 0.00020 | 5.7015 | 324.9782 | 74.7109 | 1.00271 | – |
| 2026 Mar 08 18:57 | 2026 Mar 08 12:12:03 | 0.8476 | 0.00019 | 5.7026 | 323.0506 | 74.7109 | 1.00271 | – |
| 2026 Mar 07 18:57 | 2026 Mar 07 10:53:38 | 0.8451 | 0.00018 | 5.7039 | 320.4376 | 74.7109 | 1.00271 | – |
| 2026 Mar 06 18:56 | 2026 Mar 06 14:35:08 | 0.8431 | 0.00017 | 5.7050 | 318.0956 | 74.7109 | 1.00271 | – |
| 2026 Mar 05 18:56 | 2026 Mar 05 14:35:38 | 0.8406 | 0.00016 | 5.7060 | 314.9381 | 74.7109 | 1.00271 | – |
| 2026 Mar 04 18:57 | 2026 Mar 04 14:06:38 | 0.8381 | 0.00014 | 5.7069 | 311.1330 | 74.7109 | 1.00271 | – |
| 2026 Mar 03 18:56 | 2026 Mar 03 11:16:49 | 0.8352 | 0.00013 | 5.7079 | 306.3498 | 74.7109 | 1.00271 | – |
| 2026 Mar 02 18:57 | 2026 Mar 02 14:18:38 | 0.8328 | 0.00015 | 5.7089 | 311.7258 | 74.7109 | 1.00271 | – |
| 2026 Mar 01 18:57 | 2026 Mar 01 11:04:38 | 0.8298 | 0.00014 | 5.7099 | 309.0692 | 74.7109 | 1.00271 | – |
| 2026 Feb 28 18:56 | 2026 Feb 28 11:23:55 | 0.8269 | 0.00013 | 5.7116 | 304.6595 | 74.7109 | 1.00271 | – |
| 2026 Feb 27 19:05 | 2026 Feb 26 21:44:37 | 0.8226 | 0.00012 | 5.7133 | 299.4238 | 74.7109 | 1.00271 | – |
| 2026 Feb 26 20:45 | 2026 Feb 26 13:13:01 | 0.8215 | 0.00011 | 5.7136 | 297.6152 | 74.7109 | 1.00271 | – |