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 Dec 17 18:58 | 2025 Dec 08 21:36:08 | 23.1542 | 0.82369 | 4.5467 | 318.5006 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 16 18:57 | 2025 Dec 08 21:36:08 | 23.1542 | 0.82369 | 4.5467 | 318.5006 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 15 18:58 | 2025 Dec 08 21:36:08 | 23.1542 | 0.82369 | 4.5467 | 318.5006 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 14 18:56 | 2025 Dec 08 21:36:08 | 23.1542 | 0.82369 | 4.5467 | 318.5006 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 13 18:56 | 2025 Dec 08 21:36:08 | 23.1542 | 0.82369 | 4.5467 | 318.5006 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 12 18:57 | 2025 Dec 08 21:36:08 | 23.1542 | 0.82369 | 4.5467 | 318.5006 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 11 18:56 | 2025 Dec 06 04:09:57 | 23.1247 | 0.82368 | 4.5783 | 317.7324 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 10 18:56 | 2025 Dec 06 04:09:57 | 23.1247 | 0.82368 | 4.5783 | 317.7324 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 09 18:56 | 2025 Dec 06 04:09:57 | 23.1247 | 0.82368 | 4.5783 | 317.7324 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 08 18:56 | 2025 Dec 06 04:09:57 | 23.1247 | 0.82368 | 4.5783 | 317.7324 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 07 18:56 | 2025 Dec 06 04:09:57 | 23.1247 | 0.82368 | 4.5783 | 317.7324 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 06 18:56 | 2025 Dec 01 15:05:48 | 23.0743 | 0.82365 | 4.6314 | 316.4395 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 05 18:57 | 2025 Dec 01 15:05:48 | 23.0743 | 0.82365 | 4.6314 | 316.4395 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 04 18:57 | 2025 Dec 01 15:05:48 | 23.0743 | 0.82365 | 4.6314 | 316.4395 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 03 18:56 | 2025 Dec 01 15:05:48 | 23.0743 | 0.82365 | 4.6314 | 316.4395 | 2.7740 | 1.10019 | 4.000 |
| 2025 Dec 02 18:56 | 2025 Dec 01 15:05:48 | 23.0743 | 0.82365 | 4.6314 | 316.4395 | 2.7740 | 1.10019 | 4.000 |
| 2025 Nov 30 18:57 | 2025 Nov 25 06:23:59 | 23.0036 | 0.82362 | 4.7064 | 314.6164 | 2.7740 | 1.10019 | 4.000 |
| 2025 Nov 29 18:56 | 2025 Nov 25 06:23:59 | 23.0036 | 0.82362 | 4.7064 | 314.6164 | 2.7740 | 1.10019 | 4.000 |
| 2025 Nov 28 18:57 | 2025 Nov 25 06:23:59 | 23.0036 | 0.82362 | 4.7064 | 314.6164 | 2.7740 | 1.10019 | 4.000 |
| 2025 Nov 27 18:57 | 2025 Nov 25 06:23:59 | 23.0036 | 0.82362 | 4.7064 | 314.6164 | 2.7740 | 1.10019 | 4.000 |
| 2025 Nov 26 18:57 | 2025 Nov 25 06:23:59 | 23.0036 | 0.82362 | 4.7064 | 314.6164 | 2.7740 | 1.10019 | 4.000 |
| 2025 Nov 25 18:57 | 2025 Nov 25 06:23:59 | 23.0036 | 0.82362 | 4.7064 | 314.6164 | 2.7740 | 1.10019 | 4.000 |
| 2025 Nov 24 18:56 | 2025 Nov 17 02:04:32 | 22.9184 | 0.82357 | 4.8033 | 312.2558 | 2.7740 | 1.10019 | 4.000 |
| 2025 Nov 23 18:57 | 2025 Nov 17 02:04:32 | 22.9184 | 0.82357 | 4.8033 | 312.2558 | 2.7740 | 1.10019 | 4.000 |
| 2025 Nov 21 18:57 | 2025 Nov 17 02:04:32 | 22.9184 | 0.82357 | 4.8033 | 312.2558 | 2.7740 | 1.10019 | 4.000 |
| 2025 Nov 20 18:56 | 2025 Nov 17 02:04:32 | 22.9184 | 0.82357 | 4.8033 | 312.2558 | 2.7740 | 1.10019 | 4.000 |