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 Jun 30 17:56 | 2025 Jun 28 00:45:11 | 7.8720 | 0.00062 | 4.0887 | 338.2907 | 21.6032 | 0.98995 | – |
| 2025 Jun 29 17:56 | 2025 Jun 28 00:45:11 | 7.8720 | 0.00062 | 4.0887 | 338.2907 | 21.6032 | 0.98995 | – |
| 2025 Jun 28 17:56 | 2025 Jun 28 00:45:11 | 7.8720 | 0.00062 | 4.0887 | 338.2907 | 21.6032 | 0.98995 | – |
| 2025 Jun 27 17:56 | 2025 Jun 21 23:17:43 | 7.8583 | 0.00063 | 4.0924 | 337.4427 | 21.6032 | 0.98995 | – |
| 2025 Jun 26 17:56 | 2025 Jun 21 23:17:43 | 7.8583 | 0.00063 | 4.0924 | 337.4427 | 21.6032 | 0.98995 | – |
| 2025 Jun 25 17:56 | 2025 Jun 21 23:17:43 | 7.8583 | 0.00063 | 4.0924 | 337.4427 | 21.6032 | 0.98995 | – |
| 2025 Jun 24 17:56 | 2025 Jun 21 23:17:43 | 7.8583 | 0.00063 | 4.0924 | 337.4427 | 21.6032 | 0.98995 | – |
| 2025 Jun 23 17:56 | 2025 Jun 21 23:17:43 | 7.8583 | 0.00063 | 4.0924 | 337.4427 | 21.6032 | 0.98995 | – |
| 2025 Jun 22 17:56 | 2025 Jun 15 21:50:34 | 7.8446 | 0.00063 | 4.0961 | 336.2158 | 21.6032 | 0.98995 | – |
| 2025 Jun 21 17:56 | 2025 Jun 15 21:50:34 | 7.8446 | 0.00063 | 4.0961 | 336.2158 | 21.6032 | 0.98995 | – |
| 2025 Jun 20 17:57 | 2025 Jun 15 21:50:34 | 7.8446 | 0.00063 | 4.0961 | 336.2158 | 21.6032 | 0.98995 | – |
| 2025 Jun 19 17:56 | 2025 Jun 15 21:50:34 | 7.8446 | 0.00063 | 4.0961 | 336.2158 | 21.6032 | 0.98995 | – |
| 2025 Jun 18 17:56 | 2025 Jun 15 21:50:34 | 7.8446 | 0.00063 | 4.0961 | 336.2158 | 21.6032 | 0.98995 | – |
| 2025 Jun 17 17:56 | 2025 Jun 15 21:50:34 | 7.8446 | 0.00063 | 4.0961 | 336.2158 | 21.6032 | 0.98995 | – |
| 2025 Jun 16 17:56 | 2025 Jun 11 20:52:04 | 7.8351 | 0.00064 | 4.0985 | 335.3392 | 21.6032 | 0.98995 | – |
| 2025 Jun 15 17:56 | 2025 Jun 11 20:52:04 | 7.8351 | 0.00064 | 4.0985 | 335.3392 | 21.6032 | 0.98995 | – |
| 2025 Jun 14 17:56 | 2025 Jun 11 20:52:04 | 7.8351 | 0.00064 | 4.0985 | 335.3392 | 21.6032 | 0.98995 | – |
| 2025 Jun 13 17:56 | 2025 Jun 11 20:52:04 | 7.8351 | 0.00064 | 4.0985 | 335.3392 | 21.6032 | 0.98995 | – |
| 2025 Jun 12 17:56 | 2025 Jun 11 20:52:04 | 7.8351 | 0.00064 | 4.0985 | 335.3392 | 21.6032 | 0.98995 | – |
| 2025 Jun 11 17:56 | 2025 Jun 04 19:09:55 | 7.8183 | 0.00065 | 4.1027 | 334.9029 | 21.6032 | 0.98995 | – |
| 2025 Jun 10 17:56 | 2025 Jun 04 19:09:55 | 7.8183 | 0.00065 | 4.1027 | 334.9029 | 21.6032 | 0.98995 | – |
| 2025 Jun 09 17:56 | 2025 Jun 04 19:09:55 | 7.8183 | 0.00065 | 4.1027 | 334.9029 | 21.6032 | 0.98995 | – |
| 2025 Jun 08 17:56 | 2025 Jun 04 19:09:55 | 7.8183 | 0.00065 | 4.1027 | 334.9029 | 21.6032 | 0.98995 | – |
| 2025 Jun 07 17:56 | 2025 Jun 04 19:09:55 | 7.8183 | 0.00065 | 4.1027 | 334.9029 | 21.6032 | 0.98995 | – |
| 2025 Jun 06 17:56 | 2025 Jun 04 19:09:55 | 7.8183 | 0.00065 | 4.1027 | 334.9029 | 21.6032 | 0.98995 | – |
| 2025 Jun 05 17:56 | 2025 May 31 18:11:24 | 7.8088 | 0.00066 | 4.1051 | 334.6225 | 21.6032 | 0.98995 | – |
| 2025 Jun 04 17:57 | 2025 May 31 18:11:24 | 7.8088 | 0.00066 | 4.1051 | 334.6225 | 21.6032 | 0.98995 | – |
| 2025 Jun 03 17:57 | 2025 May 31 18:11:24 | 7.8088 | 0.00066 | 4.1051 | 334.6225 | 21.6032 | 0.98995 | – |