Orbital elements of DELTA 1 R/B(2)
| Launched | 26 August 1975 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 8134 |
| 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 |
| 2025 Nov 08 18:56 | 2025 Nov 02 09:35:51 | 13.2573 | 0.71147 | 7.9184 | 8.8059 | 358.9985 | 2.41437 | – |
| 2025 Nov 07 18:57 | 2025 Nov 02 09:35:51 | 13.2573 | 0.71147 | 7.9184 | 8.8059 | 358.9985 | 2.41437 | – |
| 2025 Nov 05 18:57 | 2025 Nov 02 09:35:51 | 13.2573 | 0.71147 | 7.9184 | 8.8059 | 358.9985 | 2.41437 | – |
| 2025 Nov 04 18:57 | 2025 Nov 02 09:35:51 | 13.2573 | 0.71147 | 7.9184 | 8.8059 | 358.9985 | 2.41437 | – |
| 2025 Nov 03 18:57 | 2025 Nov 02 09:35:51 | 13.2573 | 0.71147 | 7.9184 | 8.8059 | 358.9985 | 2.41437 | – |
| 2025 Nov 02 18:57 | 2025 Oct 29 06:12:09 | 13.2445 | 0.71157 | 8.0330 | 5.5025 | 358.9985 | 2.41437 | – |
| 2025 Nov 01 18:58 | 2025 Oct 29 06:12:09 | 13.2445 | 0.71157 | 8.0330 | 5.5025 | 358.9985 | 2.41437 | – |
| 2025 Oct 31 18:57 | 2025 Oct 29 06:12:09 | 13.2445 | 0.71157 | 8.0330 | 5.5025 | 358.9985 | 2.41437 | – |
| 2025 Oct 30 18:57 | 2025 Oct 29 06:12:09 | 13.2445 | 0.71157 | 8.0330 | 5.5025 | 358.9985 | 2.41437 | – |
| 2025 Oct 29 18:57 | 2025 Oct 29 06:12:09 | 13.2445 | 0.71157 | 8.0330 | 5.5025 | 358.9985 | 2.41437 | – |
| 2025 Oct 28 18:57 | 2025 Oct 23 01:06:34 | 13.2259 | 0.71168 | 8.2051 | 0.5472 | 358.9985 | 2.41437 | – |
| 2025 Oct 27 18:57 | 2025 Oct 23 01:06:34 | 13.2259 | 0.71168 | 8.2051 | 0.5472 | 358.9985 | 2.41437 | – |
| 2025 Oct 26 18:57 | 2025 Oct 23 01:06:34 | 13.2259 | 0.71168 | 8.2051 | 0.5472 | 358.9985 | 2.41437 | – |
| 2025 Oct 25 17:57 | 2025 Oct 23 01:06:34 | 13.2259 | 0.71168 | 8.2051 | 0.5472 | 358.9985 | 2.41437 | – |
| 2025 Oct 24 17:57 | 2025 Oct 23 01:06:34 | 13.2259 | 0.71168 | 8.2051 | 0.5472 | 358.9985 | 2.41437 | – |
| 2025 Oct 22 17:56 | 2025 Oct 18 01:50:03 | 13.2120 | 0.71179 | 8.3432 | 356.5783 | 358.9985 | 2.41437 | – |
| 2025 Oct 21 17:56 | 2025 Oct 18 01:50:03 | 13.2120 | 0.71179 | 8.3432 | 356.5783 | 358.9985 | 2.41437 | – |
| 2025 Oct 20 17:56 | 2025 Oct 18 01:50:03 | 13.2120 | 0.71179 | 8.3432 | 356.5783 | 358.9985 | 2.41437 | – |
| 2025 Oct 19 17:56 | 2025 Oct 18 01:50:03 | 13.2120 | 0.71179 | 8.3432 | 356.5783 | 358.9985 | 2.41437 | – |
| 2025 Oct 18 17:56 | 2025 Oct 18 01:50:03 | 13.2120 | 0.71179 | 8.3432 | 356.5783 | 358.9985 | 2.41437 | – |
| 2025 Oct 17 17:56 | 2025 Oct 07 07:23:45 | 13.1768 | 0.71204 | 8.6448 | 347.9319 | 358.9985 | 2.41437 | – |
| 2025 Oct 16 17:56 | 2025 Oct 07 07:23:45 | 13.1768 | 0.71204 | 8.6448 | 347.9319 | 358.9985 | 2.41437 | – |
| 2025 Oct 15 17:56 | 2025 Oct 07 07:23:45 | 13.1768 | 0.71204 | 8.6448 | 347.9319 | 358.9985 | 2.41437 | – |
| 2025 Oct 14 17:56 | 2025 Oct 07 07:23:45 | 13.1768 | 0.71204 | 8.6448 | 347.9319 | 358.9985 | 2.41437 | – |
| 2025 Oct 12 17:56 | 2025 Oct 07 07:23:45 | 13.1768 | 0.71204 | 8.6448 | 347.9319 | 358.9985 | 2.41437 | – |