See also

Orbital elements of DELTA 2 R/B(1)

Launched 6 February 1999
Flight ended –
Launch site Air Force Eastern Test Range, Florida, USA
Owner United States
NORAD ID 25619

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 Jun 30 17:56 2025 Jun 28 14:10:18 22.4594 0.18553 5.9578 286.3475 54.1636 11.74223 5.243
2025 Jun 29 17:56 2025 Jun 28 14:10:18 22.4594 0.18553 5.9578 286.3475 54.1636 11.74223 5.243
2025 Jun 28 17:56 2025 Jun 28 14:10:18 22.4594 0.18553 5.9578 286.3475 54.1636 11.74223 5.243
2025 Jun 27 17:56 2025 Jun 23 03:34:20 22.4574 0.18560 7.4618 246.4148 54.1636 11.74223 5.243
2025 Jun 26 17:56 2025 Jun 23 03:34:20 22.4574 0.18560 7.4618 246.4148 54.1636 11.74223 5.243
2025 Jun 25 17:56 2025 Jun 23 03:34:20 22.4574 0.18560 7.4618 246.4148 54.1636 11.74223 5.243
2025 Jun 24 17:56 2025 Jun 23 03:34:20 22.4574 0.18560 7.4618 246.4148 54.1636 11.74223 5.243
2025 Jun 23 17:56 2025 Jun 23 03:34:20 22.4574 0.18560 7.4618 246.4148 54.1636 11.74223 5.243
2025 Jun 22 17:56 2025 Jun 17 08:51:19 22.4487 0.18568 9.0602 203.9789 54.1636 11.74223 5.243
2025 Jun 21 17:56 2025 Jun 17 08:51:19 22.4487 0.18568 9.0602 203.9789 54.1636 11.74223 5.243
2025 Jun 20 17:57 2025 Jun 17 08:51:19 22.4487 0.18568 9.0602 203.9789 54.1636 11.74223 5.243
2025 Jun 19 17:56 2025 Jun 17 08:51:19 22.4487 0.18568 9.0602 203.9789 54.1636 11.74223 5.243
2025 Jun 18 17:56 2025 Jun 17 08:51:19 22.4487 0.18568 9.0602 203.9789 54.1636 11.74223 5.243
2025 Jun 17 17:56 2025 Jun 17 08:51:19 22.4487 0.18568 9.0602 203.9789 54.1636 11.74223 5.243
2025 Jun 16 17:56 2025 Jun 11 22:18:38 22.4397 0.18578 10.5649 164.0368 54.1636 11.74223 5.243
2025 Jun 15 17:56 2025 Jun 11 22:18:38 22.4397 0.18578 10.5649 164.0368 54.1636 11.74223 5.243
2025 Jun 14 17:56 2025 Jun 11 22:18:38 22.4397 0.18578 10.5649 164.0368 54.1636 11.74223 5.243
2025 Jun 13 17:56 2025 Jun 11 22:18:38 22.4397 0.18578 10.5649 164.0368 54.1636 11.74223 5.243
2025 Jun 12 17:56 2025 Jun 11 22:18:38 22.4397 0.18578 10.5649 164.0368 54.1636 11.74223 5.243
2025 Jun 11 17:56 2025 Jun 06 09:40:20 22.4376 0.18590 12.0938 123.4791 54.1636 11.74223 5.243
2025 Jun 10 17:56 2025 Jun 06 09:40:20 22.4376 0.18590 12.0938 123.4791 54.1636 11.74223 5.243
2025 Jun 09 17:56 2025 Jun 06 09:40:20 22.4376 0.18590 12.0938 123.4791 54.1636 11.74223 5.243
2025 Jun 08 17:56 2025 Jun 06 09:40:20 22.4376 0.18590 12.0938 123.4791 54.1636 11.74223 5.243
2025 Jun 07 17:56 2025 Jun 06 09:40:20 22.4376 0.18590 12.0938 123.4791 54.1636 11.74223 5.243
2025 Jun 06 17:56 2025 Jun 06 09:40:20 22.4376 0.18590 12.0938 123.4791 54.1636 11.74223 5.243
2025 Jun 05 17:56 2025 Jun 01 13:17:08 22.4375 0.18604 13.4348 87.9144 54.1636 11.74223 5.243
2025 Jun 04 17:57 2025 Jun 01 13:17:08 22.4375 0.18604 13.4348 87.9144 54.1636 11.74223 5.243
2025 Jun 03 17:57 2025 Jun 01 13:17:08 22.4375 0.18604 13.4348 87.9144 54.1636 11.74223 5.243

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