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 Sep 15 17:56 | 2025 Sep 14 16:11:06 | 8.5465 | 0.00082 | 4.0030 | 293.0695 | 66.9546 | 0.98915 | 3.243 |
2025 Sep 12 17:57 | 2025 Sep 02 13:02:08 | 8.5179 | 0.00083 | 4.0110 | 294.0098 | 66.9546 | 0.98915 | 3.243 |
2025 Sep 11 17:57 | 2025 Sep 02 13:02:08 | 8.5179 | 0.00083 | 4.0110 | 294.0098 | 66.9546 | 0.98915 | 3.243 |
2025 Sep 10 17:56 | 2025 Sep 02 13:02:08 | 8.5179 | 0.00083 | 4.0110 | 294.0098 | 66.9546 | 0.98915 | 3.243 |
2025 Sep 08 17:57 | 2025 Sep 02 13:02:08 | 8.5179 | 0.00083 | 4.0110 | 294.0098 | 66.9546 | 0.98915 | 3.243 |
2025 Sep 07 17:56 | 2025 Sep 02 13:02:08 | 8.5179 | 0.00083 | 4.0110 | 294.0098 | 66.9546 | 0.98915 | 3.243 |
2025 Sep 06 20:41 | 2025 Sep 02 13:02:08 | 8.5179 | 0.00083 | 4.0110 | 294.0098 | 66.9546 | 0.98915 | 3.243 |
2025 Sep 03 17:57 | 2025 Sep 02 13:02:08 | 8.5179 | 0.00083 | 4.0110 | 294.0098 | 66.9546 | 0.98915 | 3.243 |
2025 Sep 02 17:56 | 2025 Aug 27 11:27:25 | 8.5031 | 0.00083 | 4.0150 | 295.2482 | 66.9546 | 0.98915 | 3.243 |
2025 Sep 01 17:56 | 2025 Aug 27 11:27:25 | 8.5031 | 0.00083 | 4.0150 | 295.2482 | 66.9546 | 0.98915 | 3.243 |
2025 Aug 31 17:56 | 2025 Aug 27 11:27:25 | 8.5031 | 0.00083 | 4.0150 | 295.2482 | 66.9546 | 0.98915 | 3.243 |
2025 Aug 30 17:56 | 2025 Aug 27 11:27:25 | 8.5031 | 0.00083 | 4.0150 | 295.2482 | 66.9546 | 0.98915 | 3.243 |
2025 Aug 29 17:56 | 2025 Aug 27 11:27:25 | 8.5031 | 0.00083 | 4.0150 | 295.2482 | 66.9546 | 0.98915 | 3.243 |
2025 Aug 28 17:57 | 2025 Aug 27 11:27:25 | 8.5031 | 0.00083 | 4.0150 | 295.2482 | 66.9546 | 0.98915 | 3.243 |
2025 Aug 27 17:56 | 2025 Aug 22 10:08:35 | 8.4909 | 0.00083 | 4.0184 | 296.4928 | 66.9546 | 0.98915 | 3.243 |
2025 Aug 26 17:56 | 2025 Aug 22 10:08:35 | 8.4909 | 0.00083 | 4.0184 | 296.4928 | 66.9546 | 0.98915 | 3.243 |
2025 Aug 25 17:56 | 2025 Aug 22 10:08:35 | 8.4909 | 0.00083 | 4.0184 | 296.4928 | 66.9546 | 0.98915 | 3.243 |
2025 Aug 24 17:56 | 2025 Aug 22 10:08:35 | 8.4909 | 0.00083 | 4.0184 | 296.4928 | 66.9546 | 0.98915 | 3.243 |
2025 Aug 23 17:56 | 2025 Aug 22 10:08:35 | 8.4909 | 0.00083 | 4.0184 | 296.4928 | 66.9546 | 0.98915 | 3.243 |
2025 Aug 22 17:56 | 2025 Aug 17 08:49:37 | 8.4791 | 0.00084 | 4.0218 | 297.5607 | 66.9546 | 0.98915 | 3.243 |
2025 Aug 20 17:56 | 2025 Aug 17 08:49:37 | 8.4791 | 0.00084 | 4.0218 | 297.5607 | 66.9546 | 0.98915 | 3.243 |