Orbital elements of DELTA 4 R/B
Launched | 28 June 2012 |
Flight ended | – |
Launch site | Air Force Eastern Test Range, Florida, USA |
Owner | United States |
NORAD ID | 38529 |
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 May 08 17:56 | 2025 May 03 05:45:35 | 6.0209 | 0.01907 | 4.2386 | 169.4552 | 190.8317 | 1.03151 | 3.243 |
2025 May 07 17:56 | 2025 May 03 05:45:35 | 6.0209 | 0.01907 | 4.2386 | 169.4552 | 190.8317 | 1.03151 | 3.243 |
2025 May 06 17:57 | 2025 May 03 05:45:35 | 6.0209 | 0.01907 | 4.2386 | 169.4552 | 190.8317 | 1.03151 | 3.243 |
2025 May 05 17:56 | 2025 May 03 05:45:35 | 6.0209 | 0.01907 | 4.2386 | 169.4552 | 190.8317 | 1.03151 | 3.243 |
2025 May 04 17:57 | 2025 May 03 05:45:35 | 6.0209 | 0.01907 | 4.2386 | 169.4552 | 190.8317 | 1.03151 | 3.243 |
2025 May 03 17:57 | 2025 May 03 05:45:35 | 6.0209 | 0.01907 | 4.2386 | 169.4552 | 190.8317 | 1.03151 | 3.243 |
2025 May 01 17:56 | 2025 Apr 21 14:34:44 | 5.9943 | 0.01907 | 4.2451 | 169.2396 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 30 17:56 | 2025 Apr 21 14:34:44 | 5.9943 | 0.01907 | 4.2451 | 169.2396 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 29 17:57 | 2025 Apr 21 14:34:44 | 5.9943 | 0.01907 | 4.2451 | 169.2396 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 27 17:56 | 2025 Apr 21 14:34:44 | 5.9943 | 0.01907 | 4.2451 | 169.2396 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 26 17:57 | 2025 Apr 21 14:34:44 | 5.9943 | 0.01907 | 4.2451 | 169.2396 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 25 17:56 | 2025 Apr 21 14:34:44 | 5.9943 | 0.01907 | 4.2451 | 169.2396 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 24 17:56 | 2025 Apr 21 14:34:44 | 5.9943 | 0.01907 | 4.2451 | 169.2396 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 23 17:57 | 2025 Apr 21 14:34:44 | 5.9943 | 0.01907 | 4.2451 | 169.2396 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 22 17:56 | 2025 Apr 21 14:34:44 | 5.9943 | 0.01907 | 4.2451 | 169.2396 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 21 17:57 | 2025 Apr 15 18:58:56 | 5.9804 | 0.01907 | 4.2483 | 169.1184 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 20 17:56 | 2025 Apr 15 18:58:56 | 5.9804 | 0.01907 | 4.2483 | 169.1184 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 19 17:56 | 2025 Apr 15 18:58:56 | 5.9804 | 0.01907 | 4.2483 | 169.1184 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 18 17:57 | 2025 Apr 15 18:58:56 | 5.9804 | 0.01907 | 4.2483 | 169.1184 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 17 17:56 | 2025 Apr 15 18:58:56 | 5.9804 | 0.01907 | 4.2483 | 169.1184 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 16 17:57 | 2025 Apr 15 18:58:56 | 5.9804 | 0.01907 | 4.2483 | 169.1184 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 15 17:56 | 2025 Apr 09 23:23:43 | 5.9662 | 0.01907 | 4.2515 | 168.9769 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 14 17:56 | 2025 Apr 09 23:23:43 | 5.9662 | 0.01907 | 4.2515 | 168.9769 | 190.8317 | 1.03151 | 3.243 |
2025 Apr 11 17:57 | 2025 Apr 09 23:23:43 | 5.9662 | 0.01907 | 4.2515 | 168.9769 | 190.8317 | 1.03151 | 3.243 |