Orbital elements of DELTA 4 R/B
| Launched | 24 May 2013 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 39169 |
| 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 02 18:57 | 2025 Oct 27 04:21:21 | 22.7136 | 0.82336 | 5.0545 | 306.1412 | 3.6129 | 1.10019 | 4.000 |
| 2025 Nov 01 18:58 | 2025 Oct 27 04:21:21 | 22.7136 | 0.82336 | 5.0545 | 306.1412 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 31 18:57 | 2025 Oct 27 04:21:21 | 22.7136 | 0.82336 | 5.0545 | 306.1412 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 30 18:57 | 2025 Oct 27 04:21:21 | 22.7136 | 0.82336 | 5.0545 | 306.1412 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 29 18:57 | 2025 Oct 27 04:21:21 | 22.7136 | 0.82336 | 5.0545 | 306.1412 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 28 18:57 | 2025 Oct 22 15:17:11 | 22.6717 | 0.82330 | 5.1097 | 304.7970 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 27 18:57 | 2025 Oct 22 15:17:11 | 22.6717 | 0.82330 | 5.1097 | 304.7970 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 26 18:57 | 2025 Oct 22 15:17:11 | 22.6717 | 0.82330 | 5.1097 | 304.7970 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 25 17:57 | 2025 Oct 22 15:17:11 | 22.6717 | 0.82330 | 5.1097 | 304.7970 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 24 17:57 | 2025 Oct 22 15:17:11 | 22.6717 | 0.82330 | 5.1097 | 304.7970 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 22 17:56 | 2025 Oct 17 04:23:47 | 22.6227 | 0.82322 | 5.1758 | 303.1838 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 21 17:56 | 2025 Oct 17 04:23:47 | 22.6227 | 0.82322 | 5.1758 | 303.1838 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 20 17:56 | 2025 Oct 17 04:23:47 | 22.6227 | 0.82322 | 5.1758 | 303.1838 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 19 17:56 | 2025 Oct 17 04:23:47 | 22.6227 | 0.82322 | 5.1758 | 303.1838 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 18 17:56 | 2025 Oct 17 04:23:47 | 22.6227 | 0.82322 | 5.1758 | 303.1838 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 17 17:56 | 2025 Oct 04 11:00:05 | 22.5135 | 0.82295 | 5.3308 | 299.4071 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 16 17:56 | 2025 Oct 04 11:00:05 | 22.5135 | 0.82295 | 5.3308 | 299.4071 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 15 17:56 | 2025 Oct 04 11:00:05 | 22.5135 | 0.82295 | 5.3308 | 299.4071 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 14 17:56 | 2025 Oct 04 11:00:05 | 22.5135 | 0.82295 | 5.3308 | 299.4071 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 12 17:56 | 2025 Oct 04 11:00:05 | 22.5135 | 0.82295 | 5.3308 | 299.4071 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 11 17:57 | 2025 Oct 04 11:00:05 | 22.5135 | 0.82295 | 5.3308 | 299.4071 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 09 17:56 | 2025 Oct 04 11:00:05 | 22.5135 | 0.82295 | 5.3308 | 299.4071 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 08 17:56 | 2025 Oct 04 11:00:05 | 22.5135 | 0.82295 | 5.3308 | 299.4071 | 3.6129 | 1.10019 | 4.000 |
| 2025 Oct 07 17:56 | 2025 Oct 04 11:00:05 | 22.5135 | 0.82295 | 5.3308 | 299.4071 | 3.6129 | 1.10019 | 4.000 |