Re: NROL-37: pre-launch elements

From: Robert Holdsworth via Seesat-l <seesat-l_at_satobs.org>
Date: Fri, 10 Jun 2016 06:08:32 +1200
Launch now rescheduled to 1855 UTC.


Webcast http://www.ulalaunch.com/webcast.aspx

Robert

On 8 June 2016 at 12:51, Ted Molczan via Seesat-l <seesat-l_at_satobs.org> wrote:
> NROL-37 is scheduled for launch from CCAFS on a Delta-IV-Heavy, on 2016 June 09. The launch period is from 17:30 to
> 22:30 UTC. Lift-off is scheduled for 17:59 UTC.
>
> http://spaceflightnow.com/2016/06/08/d374_journal/
>
> The launch azimuth indicates a GEO mission, which for an NRO heavy-lift launch, means the second stage will perform
> three burns to place the payload directly into an inclined GEO orbit.
>
> The payload probably is Mentor 7 (aka Advanced Orion 7).
>
> Below are estimated orbital elements, based on an on-time launch. Epoch corresponds to the approximate end of a burn.
>
> SECO 1                                                   190 X 244 km
> 1 77799U 77799A   16161.75819212  .00656932  00000-0  21234-3 0    07
> 2 77799  28.7000 350.7368 0040859  90.0000  38.0000 16.22456322    09
>
> SECO 2                                                 212 X 35809 km
> 1 77799U 77799A   16161.76697919  .00000000  00000-0  00000-0 0    00
> 2 77799  26.5000 350.6682 7298000 180.0000   0.0000  2.28000000    01
>
> SECO 3                                               35746 X 35830 km
> 1 77799U 77799A   16161.98567123  .00000000  00000-0  00000-0 0    07
> 2 77799   5.0000 350.5864 0010000 180.1373 179.8600  1.00270000    02
>
> Allow for cross-track errors of at least several degrees, and time errors of several minutes.
>
> The longitude at insertion into GEO will be close to 96 E. Contrary to the SECO 3 TLE, the mean motion is likely to be
> somewhat more or less than synchronous, depending whether the planned destination is east or west of 96 E. Inclination
> in GEO could be between about 3 and 7 deg.
>
> Estimated standard visual magnitude in LEO and GTO is 4 +/-2 (1000 km range, 90 deg phase angle). Once fully deployed in
> GEO, the payload will typically be near magnitude 8. The Delta IV 5m 2nd stage typically reaches mag 9 to 12 at GEO
> range.
>
> Ted Molczan
>
>
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Received on Thu Jun 09 2016 - 13:09:55 UTC

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