Orbital elements of DELTA 4 R/B
| Launched | 18 August 2016 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 41746 |
| 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 05 18:57 | 2025 Nov 02 07:23:05 | 8.1755 | 0.00046 | 4.0084 | 325.1156 | 34.8241 | 0.98991 | – |
| 2025 Nov 04 18:57 | 2025 Nov 02 07:23:05 | 8.1755 | 0.00046 | 4.0084 | 325.1156 | 34.8241 | 0.98991 | – |
| 2025 Nov 03 18:57 | 2025 Nov 02 07:23:05 | 8.1755 | 0.00046 | 4.0084 | 325.1156 | 34.8241 | 0.98991 | – |
| 2025 Nov 02 18:57 | 2025 Oct 29 06:24:40 | 8.1658 | 0.00045 | 4.0108 | 325.6306 | 34.8241 | 0.98991 | – |
| 2025 Nov 01 18:58 | 2025 Oct 29 06:24:40 | 8.1658 | 0.00045 | 4.0108 | 325.6306 | 34.8241 | 0.98991 | – |
| 2025 Oct 31 18:57 | 2025 Oct 29 06:24:40 | 8.1658 | 0.00045 | 4.0108 | 325.6306 | 34.8241 | 0.98991 | – |
| 2025 Oct 30 18:57 | 2025 Oct 29 06:24:40 | 8.1658 | 0.00045 | 4.0108 | 325.6306 | 34.8241 | 0.98991 | – |
| 2025 Oct 29 18:57 | 2025 Oct 29 06:24:40 | 8.1658 | 0.00045 | 4.0108 | 325.6306 | 34.8241 | 0.98991 | – |
| 2025 Oct 28 18:57 | 2025 Oct 23 04:57:05 | 8.1508 | 0.00044 | 4.0145 | 327.0930 | 34.8241 | 0.98991 | – |
| 2025 Oct 27 18:57 | 2025 Oct 23 04:57:05 | 8.1508 | 0.00044 | 4.0145 | 327.0930 | 34.8241 | 0.98991 | – |
| 2025 Oct 26 18:57 | 2025 Oct 23 04:57:05 | 8.1508 | 0.00044 | 4.0145 | 327.0930 | 34.8241 | 0.98991 | – |
| 2025 Oct 25 17:57 | 2025 Oct 23 04:57:05 | 8.1508 | 0.00044 | 4.0145 | 327.0930 | 34.8241 | 0.98991 | – |
| 2025 Oct 24 17:57 | 2025 Oct 23 04:57:05 | 8.1508 | 0.00044 | 4.0145 | 327.0930 | 34.8241 | 0.98991 | – |
| 2025 Oct 22 17:56 | 2025 Oct 18 03:44:32 | 8.1380 | 0.00045 | 4.0175 | 329.5616 | 34.8241 | 0.98991 | – |
| 2025 Oct 21 17:56 | 2025 Oct 18 03:44:32 | 8.1380 | 0.00045 | 4.0175 | 329.5616 | 34.8241 | 0.98991 | – |
| 2025 Oct 20 17:56 | 2025 Oct 18 03:44:32 | 8.1380 | 0.00045 | 4.0175 | 329.5616 | 34.8241 | 0.98991 | – |
| 2025 Oct 19 17:56 | 2025 Oct 18 03:44:32 | 8.1380 | 0.00045 | 4.0175 | 329.5616 | 34.8241 | 0.98991 | – |
| 2025 Oct 18 17:56 | 2025 Oct 18 03:44:32 | 8.1380 | 0.00045 | 4.0175 | 329.5616 | 34.8241 | 0.98991 | – |
| 2025 Oct 17 17:56 | 2025 Oct 07 01:04:38 | 8.1115 | 0.00046 | 4.0244 | 332.2729 | 34.8241 | 0.98991 | – |
| 2025 Oct 16 17:56 | 2025 Oct 07 01:04:38 | 8.1115 | 0.00046 | 4.0244 | 332.2729 | 34.8241 | 0.98991 | – |
| 2025 Oct 15 17:56 | 2025 Oct 07 01:04:38 | 8.1115 | 0.00046 | 4.0244 | 332.2729 | 34.8241 | 0.98991 | – |
| 2025 Oct 14 17:56 | 2025 Oct 07 01:04:38 | 8.1115 | 0.00046 | 4.0244 | 332.2729 | 34.8241 | 0.98991 | – |
| 2025 Oct 12 17:56 | 2025 Oct 07 01:04:38 | 8.1115 | 0.00046 | 4.0244 | 332.2729 | 34.8241 | 0.98991 | – |
| 2025 Oct 11 17:57 | 2025 Oct 07 01:04:38 | 8.1115 | 0.00046 | 4.0244 | 332.2729 | 34.8241 | 0.98991 | – |
| 2025 Oct 09 17:56 | 2025 Oct 07 01:04:38 | 8.1115 | 0.00046 | 4.0244 | 332.2729 | 34.8241 | 0.98991 | – |