Orbital elements of DODECAPOLE 2
Launched | 12 August 1965 |
Flight ended | – |
Launch site | Air Force Western Test Range, California, USA |
Owner | United States |
NORAD ID | 1510 |
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 Apr 02 17:57 | 2025 Apr 01 12:25:42 | 90.0567 | 0.00368 | 1.4692 | 147.0338 | 213.3149 | 14.07419 | 8.743 |
2025 Apr 01 17:56 | 2025 Apr 01 12:25:42 | 90.0567 | 0.00368 | 1.4692 | 147.0338 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 31 17:56 | 2025 Mar 26 04:33:36 | 90.0556 | 0.00356 | 1.4665 | 167.2810 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 30 17:57 | 2025 Mar 26 04:33:36 | 90.0556 | 0.00356 | 1.4665 | 167.2810 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 29 18:56 | 2025 Mar 26 04:33:36 | 90.0556 | 0.00356 | 1.4665 | 167.2810 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 28 18:57 | 2025 Mar 26 04:33:36 | 90.0556 | 0.00356 | 1.4665 | 167.2810 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 27 18:56 | 2025 Mar 26 04:33:36 | 90.0556 | 0.00356 | 1.4665 | 167.2810 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 26 18:57 | 2025 Mar 26 04:33:36 | 90.0556 | 0.00356 | 1.4665 | 167.2810 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 25 18:57 | 2025 Mar 21 08:30:59 | 90.0554 | 0.00347 | 1.4646 | 183.0688 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 24 18:57 | 2025 Mar 21 08:30:59 | 90.0554 | 0.00347 | 1.4646 | 183.0688 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 23 18:58 | 2025 Mar 21 08:30:59 | 90.0554 | 0.00347 | 1.4646 | 183.0688 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 22 18:58 | 2025 Mar 21 08:30:59 | 90.0554 | 0.00347 | 1.4646 | 183.0688 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 21 18:57 | 2025 Mar 21 08:30:59 | 90.0554 | 0.00347 | 1.4646 | 183.0688 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 20 18:57 | 2025 Mar 16 14:10:12 | 90.0564 | 0.00340 | 1.4626 | 199.2449 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 19 18:57 | 2025 Mar 16 14:10:12 | 90.0564 | 0.00340 | 1.4626 | 199.2449 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 18 18:56 | 2025 Mar 16 14:10:12 | 90.0564 | 0.00340 | 1.4626 | 199.2449 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 17 18:56 | 2025 Mar 16 14:10:12 | 90.0564 | 0.00340 | 1.4626 | 199.2449 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 16 18:56 | 2025 Mar 16 14:10:12 | 90.0564 | 0.00340 | 1.4626 | 199.2449 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 15 18:56 | 2025 Mar 10 11:23:08 | 90.0553 | 0.00336 | 1.4601 | 220.9387 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 14 18:56 | 2025 Mar 10 11:23:08 | 90.0553 | 0.00336 | 1.4601 | 220.9387 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 13 18:57 | 2025 Mar 10 11:23:08 | 90.0553 | 0.00336 | 1.4601 | 220.9387 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 11 18:56 | 2025 Mar 10 11:23:08 | 90.0553 | 0.00336 | 1.4601 | 220.9387 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 10 18:56 | 2025 Mar 10 11:23:08 | 90.0553 | 0.00336 | 1.4601 | 220.9387 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 09 18:57 | 2025 Mar 05 08:29:22 | 90.0557 | 0.00339 | 1.4581 | 239.1645 | 213.3149 | 14.07419 | 8.743 |
2025 Mar 07 18:56 | 2025 Mar 05 08:29:22 | 90.0557 | 0.00339 | 1.4581 | 239.1645 | 213.3149 | 14.07419 | 8.743 |