Orbital elements of DELTA 1 R/B
| Launched | 9 November 1967 |
| Flight ended | – |
| Launch site | Air Force Western Test Range, California, USA |
| Owner | United States |
| NORAD ID | 3036 |
| 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 04 18:57 | 2025 Nov 02 12:05:29 | 102.0143 | 0.00480 | 2.6500 | 211.1246 | 160.4377 | 12.54135 | 8.743 |
| 2025 Nov 03 18:57 | 2025 Nov 02 12:05:29 | 102.0143 | 0.00480 | 2.6500 | 211.1246 | 160.4377 | 12.54135 | 8.743 |
| 2025 Nov 02 18:57 | 2025 Oct 29 12:21:48 | 102.0142 | 0.00480 | 2.3806 | 218.7631 | 160.4377 | 12.54135 | 8.743 |
| 2025 Nov 01 18:58 | 2025 Oct 29 12:21:48 | 102.0142 | 0.00480 | 2.3806 | 218.7631 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 31 18:57 | 2025 Oct 29 12:21:48 | 102.0142 | 0.00480 | 2.3806 | 218.7631 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 30 18:57 | 2025 Oct 29 12:21:48 | 102.0142 | 0.00480 | 2.3806 | 218.7631 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 29 18:57 | 2025 Oct 29 12:21:48 | 102.0142 | 0.00480 | 2.3806 | 218.7631 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 28 18:57 | 2025 Oct 23 12:46:43 | 102.0143 | 0.00480 | 1.9766 | 230.1885 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 27 18:57 | 2025 Oct 23 12:46:43 | 102.0143 | 0.00480 | 1.9766 | 230.1885 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 26 18:57 | 2025 Oct 23 12:46:43 | 102.0143 | 0.00480 | 1.9766 | 230.1885 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 25 17:57 | 2025 Oct 23 12:46:43 | 102.0143 | 0.00480 | 1.9766 | 230.1885 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 24 17:57 | 2025 Oct 23 12:46:43 | 102.0143 | 0.00480 | 1.9766 | 230.1885 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 22 17:56 | 2025 Oct 18 06:28:38 | 102.0143 | 0.00479 | 1.6212 | 240.2624 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 21 17:56 | 2025 Oct 18 06:28:38 | 102.0143 | 0.00479 | 1.6212 | 240.2624 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 20 17:56 | 2025 Oct 18 06:28:38 | 102.0143 | 0.00479 | 1.6212 | 240.2624 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 19 17:56 | 2025 Oct 18 06:28:38 | 102.0143 | 0.00479 | 1.6212 | 240.2624 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 18 17:56 | 2025 Oct 18 06:28:38 | 102.0143 | 0.00479 | 1.6212 | 240.2624 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 17 17:56 | 2025 Oct 07 11:57:55 | 102.0142 | 0.00478 | 0.8939 | 260.8969 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 16 17:56 | 2025 Oct 07 11:57:55 | 102.0142 | 0.00478 | 0.8939 | 260.8969 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 15 17:56 | 2025 Oct 07 11:57:55 | 102.0142 | 0.00478 | 0.8939 | 260.8969 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 14 17:56 | 2025 Oct 07 11:57:55 | 102.0142 | 0.00478 | 0.8939 | 260.8969 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 12 17:56 | 2025 Oct 07 11:57:55 | 102.0142 | 0.00478 | 0.8939 | 260.8969 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 11 17:57 | 2025 Oct 07 11:57:55 | 102.0142 | 0.00478 | 0.8939 | 260.8969 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 09 17:56 | 2025 Oct 07 11:57:55 | 102.0142 | 0.00478 | 0.8939 | 260.8969 | 160.4377 | 12.54135 | 8.743 |
| 2025 Oct 08 17:56 | 2025 Oct 07 11:57:55 | 102.0142 | 0.00478 | 0.8939 | 260.8969 | 160.4377 | 12.54135 | 8.743 |