See also

Orbital elements of DELTA 1 R/B

Launched 9 July 1962
Flight ended –
Launch site Air Force Eastern Test Range, Florida, USA
Owner United States
NORAD ID 341

Show orbit between:

Start date

End date

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 Jul 11 17:56 2025 Jul 06 20:29:43 44.8002 0.24265 9.3466 292.1252 53.1658 9.14322 7.243
2025 Jul 10 17:56 2025 Jul 06 20:29:43 44.8002 0.24265 9.3466 292.1252 53.1658 9.14322 7.243
2025 Jul 09 17:56 2025 Jul 06 20:29:43 44.8002 0.24265 9.3466 292.1252 53.1658 9.14322 7.243
2025 Jul 08 17:56 2025 Jul 02 22:02:11 44.8003 0.24266 9.8364 284.2787 53.1658 9.14322 7.243
2025 Jul 07 17:56 2025 Jul 02 22:02:11 44.8003 0.24266 9.8364 284.2787 53.1658 9.14322 7.243
2025 Jul 06 17:56 2025 Jul 02 22:02:11 44.8003 0.24266 9.8364 284.2787 53.1658 9.14322 7.243
2025 Jul 05 17:56 2025 Jul 02 22:02:11 44.8003 0.24266 9.8364 284.2787 53.1658 9.14322 7.243
2025 Jul 04 17:56 2025 Jul 02 22:02:11 44.8003 0.24266 9.8364 284.2787 53.1658 9.14322 7.243
2025 Jul 03 17:56 2025 Jul 02 22:02:11 44.8003 0.24266 9.8364 284.2787 53.1658 9.14322 7.243
2025 Jul 02 17:56 2025 Jun 28 09:24:55 44.8001 0.24268 10.3997 275.2554 53.1658 9.14322 7.243
2025 Jul 01 17:56 2025 Jun 28 09:24:55 44.8001 0.24268 10.3997 275.2554 53.1658 9.14322 7.243
2025 Jun 30 17:56 2025 Jun 28 09:24:55 44.8001 0.24268 10.3997 275.2554 53.1658 9.14322 7.243
2025 Jun 29 17:56 2025 Jun 28 09:24:55 44.8001 0.24268 10.3997 275.2554 53.1658 9.14322 7.243
2025 Jun 28 17:56 2025 Jun 28 09:24:55 44.8001 0.24268 10.3997 275.2554 53.1658 9.14322 7.243
2025 Jun 27 17:56 2025 Jun 22 08:59:48 44.7990 0.24268 11.1486 263.2587 53.1658 9.14322 7.243
2025 Jun 26 17:56 2025 Jun 22 08:59:48 44.7990 0.24268 11.1486 263.2587 53.1658 9.14322 7.243
2025 Jun 25 17:56 2025 Jun 22 08:59:48 44.7990 0.24268 11.1486 263.2587 53.1658 9.14322 7.243
2025 Jun 24 17:56 2025 Jun 22 08:59:48 44.7990 0.24268 11.1486 263.2587 53.1658 9.14322 7.243
2025 Jun 23 17:56 2025 Jun 22 08:59:48 44.7990 0.24268 11.1486 263.2587 53.1658 9.14322 7.243
2025 Jun 22 17:56 2025 Jun 16 19:21:04 44.7980 0.24266 11.8418 252.1539 53.1658 9.14322 7.243
2025 Jun 21 17:56 2025 Jun 16 19:21:04 44.7980 0.24266 11.8418 252.1539 53.1658 9.14322 7.243
2025 Jun 20 17:57 2025 Jun 16 19:21:04 44.7980 0.24266 11.8418 252.1539 53.1658 9.14322 7.243
2025 Jun 19 17:56 2025 Jun 16 19:21:04 44.7980 0.24266 11.8418 252.1539 53.1658 9.14322 7.243
2025 Jun 18 17:56 2025 Jun 16 19:21:04 44.7980 0.24266 11.8418 252.1539 53.1658 9.14322 7.243
2025 Jun 17 17:56 2025 Jun 16 19:21:04 44.7980 0.24266 11.8418 252.1539 53.1658 9.14322 7.243
2025 Jun 16 17:56 2025 Jun 11 18:39:46 44.7971 0.24264 12.4677 242.1256 53.1658 9.14322 7.243
2025 Jun 15 17:56 2025 Jun 11 18:39:46 44.7971 0.24264 12.4677 242.1256 53.1658 9.14322 7.243
2025 Jun 14 17:56 2025 Jun 11 18:39:46 44.7971 0.24264 12.4677 242.1256 53.1658 9.14322 7.243

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