Orbital elements of DELTA 1 R/B
| Launched | 10 December 1972 |
| Flight ended | – |
| Launch site | Air Force Western Test Range, California, USA |
| Owner | United States |
| NORAD ID | 6306 |
| 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 Nov 18 18:57 | 2025 Nov 08 16:32:50 | 99.8319 | 0.02701 | 1.7844 | 27.5924 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 16 18:58 | 2025 Nov 08 16:32:50 | 99.8319 | 0.02701 | 1.7844 | 27.5924 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 15 18:57 | 2025 Nov 08 16:32:50 | 99.8319 | 0.02701 | 1.7844 | 27.5924 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 13 18:56 | 2025 Nov 08 16:32:50 | 99.8319 | 0.02701 | 1.7844 | 27.5924 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 12 18:57 | 2025 Nov 08 16:32:50 | 99.8319 | 0.02701 | 1.7844 | 27.5924 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 11 18:55 | 2025 Nov 08 16:32:50 | 99.8319 | 0.02701 | 1.7844 | 27.5924 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 10 18:57 | 2025 Nov 08 16:32:50 | 99.8319 | 0.02701 | 1.7844 | 27.5924 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 09 18:57 | 2025 Nov 08 16:32:50 | 99.8319 | 0.02701 | 1.7844 | 27.5924 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 08 18:56 | 2025 Nov 02 10:44:59 | 99.8325 | 0.02702 | 1.4157 | 41.4309 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 07 18:57 | 2025 Nov 02 10:44:59 | 99.8325 | 0.02702 | 1.4157 | 41.4309 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 05 18:57 | 2025 Nov 02 10:44:59 | 99.8325 | 0.02702 | 1.4157 | 41.4309 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 04 18:57 | 2025 Nov 02 10:44:59 | 99.8325 | 0.02702 | 1.4157 | 41.4309 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 03 18:57 | 2025 Nov 02 10:44:59 | 99.8325 | 0.02702 | 1.4157 | 41.4309 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 02 18:57 | 2025 Oct 28 15:56:54 | 99.8327 | 0.02703 | 1.1331 | 52.0165 | 123.2840 | 12.88490 | 6.743 |
| 2025 Nov 01 18:58 | 2025 Oct 28 15:56:54 | 99.8327 | 0.02703 | 1.1331 | 52.0165 | 123.2840 | 12.88490 | 6.743 |
| 2025 Oct 31 18:57 | 2025 Oct 28 15:56:54 | 99.8327 | 0.02703 | 1.1331 | 52.0165 | 123.2840 | 12.88490 | 6.743 |
| 2025 Oct 30 18:57 | 2025 Oct 28 15:56:54 | 99.8327 | 0.02703 | 1.1331 | 52.0165 | 123.2840 | 12.88490 | 6.743 |
| 2025 Oct 29 18:57 | 2025 Oct 28 15:56:54 | 99.8327 | 0.02703 | 1.1331 | 52.0165 | 123.2840 | 12.88490 | 6.743 |
| 2025 Oct 28 18:57 | 2025 Oct 23 16:30:13 | 99.8333 | 0.02703 | 0.8391 | 63.0397 | 123.2840 | 12.88490 | 6.743 |
| 2025 Oct 27 18:57 | 2025 Oct 23 16:30:13 | 99.8333 | 0.02703 | 0.8391 | 63.0397 | 123.2840 | 12.88490 | 6.743 |
| 2025 Oct 26 18:57 | 2025 Oct 23 16:30:13 | 99.8333 | 0.02703 | 0.8391 | 63.0397 | 123.2840 | 12.88490 | 6.743 |
| 2025 Oct 25 17:57 | 2025 Oct 23 16:30:13 | 99.8333 | 0.02703 | 0.8391 | 63.0397 | 123.2840 | 12.88490 | 6.743 |
| 2025 Oct 24 17:57 | 2025 Oct 23 16:30:13 | 99.8333 | 0.02703 | 0.8391 | 63.0397 | 123.2840 | 12.88490 | 6.743 |
| 2025 Oct 22 17:56 | 2025 Oct 18 05:29:03 | 99.8341 | 0.02704 | 0.5166 | 75.1256 | 123.2840 | 12.88490 | 6.743 |