Orbital elements of DELTA 1 R/B(2)
Launched | 25 October 1966 |
Flight ended | – |
Launch site | Air Force Eastern Test Range, Florida, USA |
Owner | United States |
NORAD ID | 11792 |
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 Oct 21 17:56 | 2025 Oct 13 18:49:43 | 17.8074 | 0.60944 | 15.9968 | 298.5825 | 13.7993 | 3.81540 | – |
2025 Oct 20 17:56 | 2025 Oct 13 18:49:43 | 17.8074 | 0.60944 | 15.9968 | 298.5825 | 13.7993 | 3.81540 | – |
2025 Oct 19 17:56 | 2025 Oct 13 18:49:43 | 17.8074 | 0.60944 | 15.9968 | 298.5825 | 13.7993 | 3.81540 | – |
2025 Oct 18 17:56 | 2025 Oct 13 18:49:43 | 17.8074 | 0.60944 | 15.9968 | 298.5825 | 13.7993 | 3.81540 | – |
2025 Oct 17 17:56 | 2025 Oct 05 22:06:31 | 17.8158 | 0.60979 | 16.3830 | 287.8479 | 13.7993 | 3.81540 | – |
2025 Oct 16 17:56 | 2025 Oct 05 22:06:31 | 17.8158 | 0.60979 | 16.3830 | 287.8479 | 13.7993 | 3.81540 | – |
2025 Oct 15 17:56 | 2025 Oct 05 22:06:31 | 17.8158 | 0.60979 | 16.3830 | 287.8479 | 13.7993 | 3.81540 | – |
2025 Oct 14 17:56 | 2025 Oct 05 22:06:31 | 17.8158 | 0.60979 | 16.3830 | 287.8479 | 13.7993 | 3.81540 | – |
2025 Oct 12 17:56 | 2025 Oct 05 22:06:31 | 17.8158 | 0.60979 | 16.3830 | 287.8479 | 13.7993 | 3.81540 | – |
2025 Oct 11 17:57 | 2025 Oct 05 22:06:31 | 17.8158 | 0.60979 | 16.3830 | 287.8479 | 13.7993 | 3.81540 | – |
2025 Oct 09 17:56 | 2025 Oct 05 22:06:31 | 17.8158 | 0.60979 | 16.3830 | 287.8479 | 13.7993 | 3.81540 | – |
2025 Oct 08 17:56 | 2025 Oct 05 22:06:31 | 17.8158 | 0.60979 | 16.3830 | 287.8479 | 13.7993 | 3.81540 | – |
2025 Oct 07 17:56 | 2025 Oct 05 22:06:31 | 17.8158 | 0.60979 | 16.3830 | 287.8479 | 13.7993 | 3.81540 | – |
2025 Oct 05 17:56 | 2025 Sep 21 05:22:36 | 17.8297 | 0.61064 | 17.1025 | 267.8068 | 13.7993 | 3.81540 | – |
2025 Oct 04 17:57 | 2025 Sep 21 05:22:36 | 17.8297 | 0.61064 | 17.1025 | 267.8068 | 13.7993 | 3.81540 | – |
2025 Oct 03 17:57 | 2025 Sep 21 05:22:36 | 17.8297 | 0.61064 | 17.1025 | 267.8068 | 13.7993 | 3.81540 | – |
2025 Oct 02 17:56 | 2025 Sep 21 05:22:36 | 17.8297 | 0.61064 | 17.1025 | 267.8068 | 13.7993 | 3.81540 | – |
2025 Sep 30 17:56 | 2025 Sep 21 05:22:36 | 17.8297 | 0.61064 | 17.1025 | 267.8068 | 13.7993 | 3.81540 | – |
2025 Sep 29 17:56 | 2025 Sep 21 05:22:36 | 17.8297 | 0.61064 | 17.1025 | 267.8068 | 13.7993 | 3.81540 | – |
2025 Sep 28 17:56 | 2025 Sep 21 05:22:36 | 17.8297 | 0.61064 | 17.1025 | 267.8068 | 13.7993 | 3.81540 | – |
2025 Sep 27 17:56 | 2025 Sep 21 05:22:36 | 17.8297 | 0.61064 | 17.1025 | 267.8068 | 13.7993 | 3.81540 | – |
2025 Sep 26 17:56 | 2025 Sep 21 05:22:36 | 17.8297 | 0.61064 | 17.1025 | 267.8068 | 13.7993 | 3.81540 | – |
2025 Sep 25 17:56 | 2025 Sep 18 14:19:11 | 17.8319 | 0.61076 | 17.2308 | 264.2331 | 13.7993 | 3.81540 | – |
2025 Sep 24 17:56 | 2025 Sep 18 14:19:11 | 17.8319 | 0.61076 | 17.2308 | 264.2331 | 13.7993 | 3.81540 | – |