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 Jun 30 17:56 | 2025 Jun 26 11:35:22 | 22.0373 | 0.81876 | 6.5191 | 270.4701 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 29 17:56 | 2025 Jun 26 11:35:22 | 22.0373 | 0.81876 | 6.5191 | 270.4701 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 28 17:56 | 2025 Jun 26 11:35:22 | 22.0373 | 0.81876 | 6.5191 | 270.4701 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 27 17:56 | 2025 Jun 20 02:54:48 | 22.0349 | 0.81847 | 6.5913 | 268.7049 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 26 17:56 | 2025 Jun 20 02:54:48 | 22.0349 | 0.81847 | 6.5913 | 268.7049 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 25 17:56 | 2025 Jun 20 02:54:48 | 22.0349 | 0.81847 | 6.5913 | 268.7049 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 24 17:56 | 2025 Jun 20 02:54:48 | 22.0349 | 0.81847 | 6.5913 | 268.7049 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 23 17:56 | 2025 Jun 20 02:54:48 | 22.0349 | 0.81847 | 6.5913 | 268.7049 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 22 17:56 | 2025 Jun 13 18:13:50 | 22.0337 | 0.81818 | 6.6636 | 266.9382 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 21 17:56 | 2025 Jun 13 18:13:50 | 22.0337 | 0.81818 | 6.6636 | 266.9382 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 20 17:57 | 2025 Jun 13 18:13:50 | 22.0337 | 0.81818 | 6.6636 | 266.9382 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 19 17:56 | 2025 Jun 13 18:13:50 | 22.0337 | 0.81818 | 6.6636 | 266.9382 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 18 17:56 | 2025 Jun 13 18:13:50 | 22.0337 | 0.81818 | 6.6636 | 266.9382 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 17 17:56 | 2025 Jun 13 18:13:50 | 22.0337 | 0.81818 | 6.6636 | 266.9382 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 16 17:56 | 2025 Jun 10 02:59:21 | 22.0354 | 0.81800 | 6.7047 | 265.9331 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 15 17:56 | 2025 Jun 10 02:59:21 | 22.0354 | 0.81800 | 6.7047 | 265.9331 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 14 17:56 | 2025 Jun 10 02:59:21 | 22.0354 | 0.81800 | 6.7047 | 265.9331 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 13 17:56 | 2025 Jun 10 02:59:21 | 22.0354 | 0.81800 | 6.7047 | 265.9331 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 12 17:56 | 2025 Jun 10 02:59:21 | 22.0354 | 0.81800 | 6.7047 | 265.9331 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 11 17:56 | 2025 Jun 04 16:07:11 | 22.0377 | 0.81778 | 6.7657 | 264.4303 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 10 17:56 | 2025 Jun 04 16:07:11 | 22.0377 | 0.81778 | 6.7657 | 264.4303 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 09 17:56 | 2025 Jun 04 16:07:11 | 22.0377 | 0.81778 | 6.7657 | 264.4303 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 08 17:56 | 2025 Jun 04 16:07:11 | 22.0377 | 0.81778 | 6.7657 | 264.4303 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 07 17:56 | 2025 Jun 04 16:07:11 | 22.0377 | 0.81778 | 6.7657 | 264.4303 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 06 17:56 | 2025 Jun 04 16:07:11 | 22.0377 | 0.81778 | 6.7657 | 264.4303 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 05 17:56 | 2025 May 31 03:03:40 | 22.0406 | 0.81760 | 6.8160 | 263.1878 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 04 17:57 | 2025 May 31 03:03:40 | 22.0406 | 0.81760 | 6.8160 | 263.1878 | 7.9869 | 1.10018 | 4.000 |
2025 Jun 03 17:57 | 2025 May 31 03:03:40 | 22.0406 | 0.81760 | 6.8160 | 263.1878 | 7.9869 | 1.10018 | 4.000 |