Re: NROL-76 launch

From: Jon . via Seesat-l <seesat-l_at_satobs.org>
Date: Mon, 1 May 2017 09:43:44 +0200
Hello all,

There are elements for a 850 circular orbit, assuming launch at 11:00 UTC:


NROL-71 scenario #1                                      858 X 858 km
1 70099U 17500B   17121.66667824 0.00000000  00000-0  00000+0 0    09
2 70099  50.0000 278.0862 0000010  73.6430 274.4981 14.10600000    06


Ted's scenarios are much more logical and fits the reality much better.


Jon.

2017-05-01 7:18 GMT+02:00 Ted Molczan via Seesat-l <seesat-l_at_satobs.org>:

> I inadvertently re-issued the Apr 30 version of the 50 deg, 300 km
> elements. Below are the May 01 elements:
>
> 1 74200U          17121.46250000  .00000000  00000-0  00000-0 0    05
> 2 74200  50.0000 279.9856 0005000 177.0000 220.5000 15.90000000    00
>
> Ted Molczan
>
>
> _______________________________________________
> Seesat-l mailing list
> http://mailman.satobs.org/mailman/listinfo/seesat-l
>



-- 
Jon, COSPAR 6242, 42.9453, -2.82839, 623m, Bitoriano, Basque Country.
_______________________________________________
Seesat-l mailing list
http://mailman.satobs.org/mailman/listinfo/seesat-l
Received on Mon May 01 2017 - 02:44:51 UTC

This archive was generated by hypermail 2.3.0 : Mon May 01 2017 - 07:44:51 UTC