Orbital elements of DELTA 4 R/B
| Launched | 27 May 2010 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 36586 |
| 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 Dec 15 18:58 | 2025 Dec 09 09:24:09 | 53.8643 | 0.02110 | 15.8499 | 158.7900 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 14 18:56 | 2025 Dec 09 09:24:09 | 53.8643 | 0.02110 | 15.8499 | 158.7900 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 13 18:56 | 2025 Dec 09 09:24:09 | 53.8643 | 0.02110 | 15.8499 | 158.7900 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 12 18:57 | 2025 Dec 09 09:24:09 | 53.8643 | 0.02110 | 15.8499 | 158.7900 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 11 18:56 | 2025 Dec 07 07:04:41 | 53.8653 | 0.02110 | 15.8550 | 158.7371 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 10 18:56 | 2025 Dec 07 07:04:41 | 53.8653 | 0.02110 | 15.8550 | 158.7371 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 09 18:56 | 2025 Dec 07 07:04:41 | 53.8653 | 0.02110 | 15.8550 | 158.7371 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 08 18:56 | 2025 Dec 07 07:04:41 | 53.8653 | 0.02110 | 15.8550 | 158.7371 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 07 18:56 | 2025 Dec 07 07:04:41 | 53.8653 | 0.02110 | 15.8550 | 158.7371 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 06 18:56 | 2025 Nov 29 10:54:38 | 53.8692 | 0.02110 | 15.8743 | 158.5077 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 05 18:57 | 2025 Nov 29 10:54:38 | 53.8692 | 0.02110 | 15.8743 | 158.5077 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 04 18:57 | 2025 Nov 29 10:54:38 | 53.8692 | 0.02110 | 15.8743 | 158.5077 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 03 18:56 | 2025 Nov 29 10:54:38 | 53.8692 | 0.02110 | 15.8743 | 158.5077 | 19.3947 | 1.90940 | 3.243 |
| 2025 Dec 02 18:56 | 2025 Nov 29 10:54:38 | 53.8692 | 0.02110 | 15.8743 | 158.5077 | 19.3947 | 1.90940 | 3.243 |
| 2025 Nov 30 18:57 | 2025 Nov 24 17:36:28 | 53.8712 | 0.02109 | 15.8858 | 158.4045 | 19.3947 | 1.90940 | 3.243 |
| 2025 Nov 29 18:56 | 2025 Nov 24 17:36:28 | 53.8712 | 0.02109 | 15.8858 | 158.4045 | 19.3947 | 1.90940 | 3.243 |
| 2025 Nov 28 18:57 | 2025 Nov 24 17:36:28 | 53.8712 | 0.02109 | 15.8858 | 158.4045 | 19.3947 | 1.90940 | 3.243 |
| 2025 Nov 27 18:57 | 2025 Nov 24 17:36:28 | 53.8712 | 0.02109 | 15.8858 | 158.4045 | 19.3947 | 1.90940 | 3.243 |
| 2025 Nov 26 18:57 | 2025 Nov 24 17:36:28 | 53.8712 | 0.02109 | 15.8858 | 158.4045 | 19.3947 | 1.90940 | 3.243 |
| 2025 Nov 25 18:57 | 2025 Nov 24 17:36:28 | 53.8712 | 0.02109 | 15.8858 | 158.4045 | 19.3947 | 1.90940 | 3.243 |
| 2025 Nov 24 18:56 | 2025 Nov 18 10:46:38 | 53.8753 | 0.02108 | 15.9012 | 158.2752 | 19.3947 | 1.90940 | 3.243 |
| 2025 Nov 23 18:57 | 2025 Nov 18 10:46:38 | 53.8753 | 0.02108 | 15.9012 | 158.2752 | 19.3947 | 1.90940 | 3.243 |
| 2025 Nov 21 18:57 | 2025 Nov 18 10:46:38 | 53.8753 | 0.02108 | 15.9012 | 158.2752 | 19.3947 | 1.90940 | 3.243 |
| 2025 Nov 20 18:56 | 2025 Nov 18 10:46:38 | 53.8753 | 0.02108 | 15.9012 | 158.2752 | 19.3947 | 1.90940 | 3.243 |
| 2025 Nov 18 18:57 | 2025 Nov 08 11:59:44 | 53.8797 | 0.02109 | 15.9256 | 158.0358 | 19.3947 | 1.90940 | 3.243 |