Orbital elements of DELTA 4 R/B
| Launched | 5 December 2009 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 36109 |
| 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 Jun 30 17:56 | 2025 Jun 27 19:51:57 | 25.6636 | 0.81628 | 23.6197 | 97.7055 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 29 17:56 | 2025 Jun 27 19:51:57 | 25.6636 | 0.81628 | 23.6197 | 97.7055 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 28 17:56 | 2025 Jun 27 19:51:57 | 25.6636 | 0.81628 | 23.6197 | 97.7055 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 27 17:56 | 2025 Jun 22 12:36:38 | 25.6657 | 0.81632 | 23.6776 | 96.1961 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 26 17:56 | 2025 Jun 22 12:36:38 | 25.6657 | 0.81632 | 23.6776 | 96.1961 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 25 17:56 | 2025 Jun 22 12:36:38 | 25.6657 | 0.81632 | 23.6776 | 96.1961 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 24 17:56 | 2025 Jun 22 12:36:38 | 25.6657 | 0.81632 | 23.6776 | 96.1961 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 23 17:56 | 2025 Jun 22 12:36:38 | 25.6657 | 0.81632 | 23.6776 | 96.1961 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 22 17:56 | 2025 Jun 15 12:40:33 | 25.6674 | 0.81634 | 23.7543 | 94.2064 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 21 17:56 | 2025 Jun 15 12:40:33 | 25.6674 | 0.81634 | 23.7543 | 94.2064 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 20 17:57 | 2025 Jun 15 12:40:33 | 25.6674 | 0.81634 | 23.7543 | 94.2064 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 19 17:56 | 2025 Jun 15 12:40:33 | 25.6674 | 0.81634 | 23.7543 | 94.2064 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 18 17:56 | 2025 Jun 15 12:40:33 | 25.6674 | 0.81634 | 23.7543 | 94.2064 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 17 17:56 | 2025 Jun 15 12:40:33 | 25.6674 | 0.81634 | 23.7543 | 94.2064 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 16 17:56 | 2025 Jun 09 14:38:21 | 25.6682 | 0.81634 | 23.8187 | 92.5342 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 15 17:56 | 2025 Jun 09 14:38:21 | 25.6682 | 0.81634 | 23.8187 | 92.5342 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 14 17:56 | 2025 Jun 09 14:38:21 | 25.6682 | 0.81634 | 23.8187 | 92.5342 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 13 17:56 | 2025 Jun 09 14:38:21 | 25.6682 | 0.81634 | 23.8187 | 92.5342 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 12 17:56 | 2025 Jun 09 14:38:21 | 25.6682 | 0.81634 | 23.8187 | 92.5342 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 11 17:56 | 2025 Jun 05 18:41:38 | 25.6687 | 0.81633 | 23.8603 | 91.4530 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 10 17:56 | 2025 Jun 05 18:41:38 | 25.6687 | 0.81633 | 23.8603 | 91.4530 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 09 17:56 | 2025 Jun 05 18:41:38 | 25.6687 | 0.81633 | 23.8603 | 91.4530 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 08 17:56 | 2025 Jun 05 18:41:38 | 25.6687 | 0.81633 | 23.8603 | 91.4530 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 07 17:56 | 2025 Jun 05 18:41:38 | 25.6687 | 0.81633 | 23.8603 | 91.4530 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 06 17:56 | 2025 Jun 05 18:41:38 | 25.6687 | 0.81633 | 23.8603 | 91.4530 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 05 17:56 | 2025 Jun 01 14:32:38 | 25.6687 | 0.81633 | 23.9056 | 90.2749 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 04 17:57 | 2025 Jun 01 14:32:38 | 25.6687 | 0.81633 | 23.9056 | 90.2749 | 255.8600 | 1.19250 | 3.500 |
| 2025 Jun 03 17:57 | 2025 Jun 01 14:32:38 | 25.6687 | 0.81633 | 23.9056 | 90.2749 | 255.8600 | 1.19250 | 3.500 |