Orbital elements of DELTA 1 R/B(1)
| Launched | 13 November 1984 |
| Flight ended | – |
| Launch site | Air Force Eastern Test Range, Florida, USA |
| Owner | United States |
| NORAD ID | 15392 |
| 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 20 17:56 | 2025 Oct 18 01:08:06 | 21.4898 | 0.10323 | 4.9728 | 77.2743 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 19 17:56 | 2025 Oct 18 01:08:06 | 21.4898 | 0.10323 | 4.9728 | 77.2743 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 18 17:56 | 2025 Oct 18 01:08:06 | 21.4898 | 0.10323 | 4.9728 | 77.2743 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 17 17:56 | 2025 Oct 07 15:07:51 | 21.4931 | 0.10323 | 8.1498 | 352.0506 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 16 17:56 | 2025 Oct 07 15:07:51 | 21.4931 | 0.10323 | 8.1498 | 352.0506 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 15 17:56 | 2025 Oct 07 15:07:51 | 21.4931 | 0.10323 | 8.1498 | 352.0506 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 14 17:56 | 2025 Oct 07 15:07:51 | 21.4931 | 0.10323 | 8.1498 | 352.0506 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 12 17:56 | 2025 Oct 07 15:07:51 | 21.4931 | 0.10323 | 8.1498 | 352.0506 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 11 17:57 | 2025 Oct 07 15:07:51 | 21.4931 | 0.10323 | 8.1498 | 352.0506 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 09 17:56 | 2025 Oct 07 15:07:51 | 21.4931 | 0.10323 | 8.1498 | 352.0506 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 08 17:56 | 2025 Oct 07 15:07:51 | 21.4931 | 0.10323 | 8.1498 | 352.0506 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 07 17:56 | 2025 Oct 07 15:07:51 | 21.4931 | 0.10323 | 8.1498 | 352.0506 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 05 17:56 | 2025 Sep 26 02:13:28 | 21.4975 | 0.10325 | 11.6667 | 257.6816 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 04 17:57 | 2025 Sep 26 02:13:28 | 21.4975 | 0.10325 | 11.6667 | 257.6816 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 03 17:57 | 2025 Sep 26 02:13:28 | 21.4975 | 0.10325 | 11.6667 | 257.6816 | 294.0900 | 12.46051 | 4.743 |
| 2025 Oct 02 17:56 | 2025 Sep 26 02:13:28 | 21.4975 | 0.10325 | 11.6667 | 257.6816 | 294.0900 | 12.46051 | 4.743 |
| 2025 Sep 30 17:56 | 2025 Sep 26 02:13:28 | 21.4975 | 0.10325 | 11.6667 | 257.6816 | 294.0900 | 12.46051 | 4.743 |
| 2025 Sep 29 17:56 | 2025 Sep 26 02:13:28 | 21.4975 | 0.10325 | 11.6667 | 257.6816 | 294.0900 | 12.46051 | 4.743 |
| 2025 Sep 28 17:56 | 2025 Sep 26 02:13:28 | 21.4975 | 0.10325 | 11.6667 | 257.6816 | 294.0900 | 12.46051 | 4.743 |
| 2025 Sep 27 17:56 | 2025 Sep 26 02:13:28 | 21.4975 | 0.10325 | 11.6667 | 257.6816 | 294.0900 | 12.46051 | 4.743 |
| 2025 Sep 26 17:56 | 2025 Sep 26 02:13:28 | 21.4975 | 0.10325 | 11.6667 | 257.6816 | 294.0900 | 12.46051 | 4.743 |
| 2025 Sep 25 17:56 | 2025 Sep 20 00:08:21 | 21.4945 | 0.10323 | 13.5221 | 207.8957 | 294.0900 | 12.46051 | 4.743 |
| 2025 Sep 24 17:56 | 2025 Sep 20 00:08:21 | 21.4945 | 0.10323 | 13.5221 | 207.8957 | 294.0900 | 12.46051 | 4.743 |