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 Aug 05 17:56 | 2025 Jul 29 04:49:16 | 22.1045 | 0.82035 | 6.1407 | 279.6915 | 6.1795 | 1.10018 | 4.000 |
| 2025 Aug 04 17:56 | 2025 Jul 29 04:49:16 | 22.1045 | 0.82035 | 6.1407 | 279.6915 | 6.1795 | 1.10018 | 4.000 |
| 2025 Aug 03 17:56 | 2025 Jul 29 04:49:16 | 22.1045 | 0.82035 | 6.1407 | 279.6915 | 6.1795 | 1.10018 | 4.000 |
| 2025 Aug 02 17:56 | 2025 Jul 29 04:49:16 | 22.1045 | 0.82035 | 6.1407 | 279.6915 | 6.1795 | 1.10018 | 4.000 |
| 2025 Aug 01 17:56 | 2025 Jul 29 04:49:16 | 22.1045 | 0.82035 | 6.1407 | 279.6915 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 31 17:56 | 2025 Jul 23 17:56:46 | 22.0869 | 0.82009 | 6.2042 | 278.1418 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 29 17:56 | 2025 Jul 23 17:56:46 | 22.0869 | 0.82009 | 6.2042 | 278.1418 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 28 17:58 | 2025 Jul 23 17:56:46 | 22.0869 | 0.82009 | 6.2042 | 278.1418 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 26 17:56 | 2025 Jul 23 17:56:46 | 22.0869 | 0.82009 | 6.2042 | 278.1418 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 25 17:56 | 2025 Jul 19 04:53:24 | 22.0747 | 0.81987 | 6.2572 | 276.8521 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 24 17:56 | 2025 Jul 19 04:53:24 | 22.0747 | 0.81987 | 6.2572 | 276.8521 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 23 17:56 | 2025 Jul 19 04:53:24 | 22.0747 | 0.81987 | 6.2572 | 276.8521 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 22 17:56 | 2025 Jul 19 04:53:24 | 22.0747 | 0.81987 | 6.2572 | 276.8521 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 21 17:56 | 2025 Jul 19 04:53:24 | 22.0747 | 0.81987 | 6.2572 | 276.8521 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 20 17:56 | 2025 Jul 19 04:53:24 | 22.0747 | 0.81987 | 6.2572 | 276.8521 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 19 17:57 | 2025 Jul 14 15:49:32 | 22.0638 | 0.81964 | 6.3102 | 275.5660 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 18 17:57 | 2025 Jul 14 15:49:32 | 22.0638 | 0.81964 | 6.3102 | 275.5660 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 17 17:56 | 2025 Jul 14 15:49:32 | 22.0638 | 0.81964 | 6.3102 | 275.5660 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 16 17:56 | 2025 Jul 14 15:49:32 | 22.0638 | 0.81964 | 6.3102 | 275.5660 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 15 17:56 | 2025 Jul 14 15:49:32 | 22.0638 | 0.81964 | 6.3102 | 275.5660 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 14 17:56 | 2025 Jul 03 18:05:11 | 22.0451 | 0.81910 | 6.4363 | 272.4964 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 13 17:56 | 2025 Jul 03 18:05:11 | 22.0451 | 0.81910 | 6.4363 | 272.4964 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 12 17:56 | 2025 Jul 03 18:05:11 | 22.0451 | 0.81910 | 6.4363 | 272.4964 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 11 17:56 | 2025 Jul 03 18:05:11 | 22.0451 | 0.81910 | 6.4363 | 272.4964 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 10 17:56 | 2025 Jul 03 18:05:11 | 22.0451 | 0.81910 | 6.4363 | 272.4964 | 6.1795 | 1.10018 | 4.000 |
| 2025 Jul 09 17:56 | 2025 Jul 03 18:05:11 | 22.0451 | 0.81910 | 6.4363 | 272.4964 | 6.1795 | 1.10018 | 4.000 |