Orbital elements of DELTA 4 R/B
| Launched | 27 July 2014 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 40102 |
| 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 11 15:00:57 | 8.7582 | 0.00095 | 3.9471 | 284.5843 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 14 18:56 | 2025 Dec 11 15:00:57 | 8.7582 | 0.00095 | 3.9471 | 284.5843 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 13 18:56 | 2025 Dec 11 15:00:57 | 8.7582 | 0.00095 | 3.9471 | 284.5843 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 12 18:57 | 2025 Dec 11 15:00:57 | 8.7582 | 0.00095 | 3.9471 | 284.5843 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 11 18:56 | 2025 Dec 05 13:26:17 | 8.7440 | 0.00095 | 3.9510 | 284.8745 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 10 18:56 | 2025 Dec 05 13:26:17 | 8.7440 | 0.00095 | 3.9510 | 284.8745 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 09 18:56 | 2025 Dec 05 13:26:17 | 8.7440 | 0.00095 | 3.9510 | 284.8745 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 08 18:56 | 2025 Dec 05 13:26:17 | 8.7440 | 0.00095 | 3.9510 | 284.8745 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 07 18:56 | 2025 Dec 05 13:26:17 | 8.7440 | 0.00095 | 3.9510 | 284.8745 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 06 18:56 | 2025 Nov 30 12:07:51 | 8.7324 | 0.00094 | 3.9542 | 284.8001 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 05 18:57 | 2025 Nov 30 12:07:51 | 8.7324 | 0.00094 | 3.9542 | 284.8001 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 04 18:57 | 2025 Nov 30 12:07:51 | 8.7324 | 0.00094 | 3.9542 | 284.8001 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 03 18:56 | 2025 Nov 30 12:07:51 | 8.7324 | 0.00094 | 3.9542 | 284.8001 | 75.2167 | 0.98912 | 3.243 |
| 2025 Dec 02 18:56 | 2025 Nov 30 12:07:51 | 8.7324 | 0.00094 | 3.9542 | 284.8001 | 75.2167 | 0.98912 | 3.243 |
| 2025 Nov 30 18:57 | 2025 Nov 25 10:49:13 | 8.7204 | 0.00093 | 3.9574 | 284.2364 | 75.2167 | 0.98912 | 3.243 |
| 2025 Nov 29 18:56 | 2025 Nov 25 10:49:13 | 8.7204 | 0.00093 | 3.9574 | 284.2364 | 75.2167 | 0.98912 | 3.243 |
| 2025 Nov 28 18:57 | 2025 Nov 25 10:49:13 | 8.7204 | 0.00093 | 3.9574 | 284.2364 | 75.2167 | 0.98912 | 3.243 |
| 2025 Nov 27 18:57 | 2025 Nov 25 10:49:13 | 8.7204 | 0.00093 | 3.9574 | 284.2364 | 75.2167 | 0.98912 | 3.243 |
| 2025 Nov 26 18:57 | 2025 Nov 25 10:49:13 | 8.7204 | 0.00093 | 3.9574 | 284.2364 | 75.2167 | 0.98912 | 3.243 |
| 2025 Nov 25 18:57 | 2025 Nov 25 10:49:13 | 8.7204 | 0.00093 | 3.9574 | 284.2364 | 75.2167 | 0.98912 | 3.243 |
| 2025 Nov 24 18:56 | 2025 Nov 19 09:14:33 | 8.7055 | 0.00091 | 3.9611 | 284.1517 | 75.2167 | 0.98912 | 3.243 |
| 2025 Nov 23 18:57 | 2025 Nov 19 09:14:33 | 8.7055 | 0.00091 | 3.9611 | 284.1517 | 75.2167 | 0.98912 | 3.243 |
| 2025 Nov 21 18:57 | 2025 Nov 19 09:14:33 | 8.7055 | 0.00091 | 3.9611 | 284.1517 | 75.2167 | 0.98912 | 3.243 |
| 2025 Nov 20 18:56 | 2025 Nov 19 09:14:33 | 8.7055 | 0.00091 | 3.9611 | 284.1517 | 75.2167 | 0.98912 | 3.243 |
| 2025 Nov 18 18:57 | 2025 Nov 08 06:20:59 | 8.6787 | 0.00089 | 3.9682 | 285.8214 | 75.2167 | 0.98912 | 3.243 |