[Isocops] IBEX Orbit# 217 Perigee Tracking Contact

[Ibex Mission Operations]

Guys,
    The tracking contact for ORbit# 217 was nominal for command/telemetry
and the inertial maneuver successful.
The LADEE tracking support was successful in achieveing autotrack from
USN/HBK

1. CAR# 638 Upload Orbit# 219 ATS  1.IBEX_2013_250_o0219a_v001.scr (539-
634,635)
2. reset_master_timer.scr<2.reset_master_timer.scr/ops_set_sc_time.scr/@FMI_SetDownlink>
3. ops_set_sc_time.scr
4. at FMI_SetDownlink (2k)
5. @FMI_SetDownlink(64k)

  IBEX Orbit# 217 PERIGEE Target Vectors 28 Aug 13

  J2000  Spin Axis

  ECI X    -0.889817

  ECI Y    0.418922

  ECI Z    0.180913



  Precession Maneuver

  MPS Diff             0.624      deg

   *MPS Diff should be < 1.5  *

  0.18395500         ActNor.EstInrToBdy[0]

  -0.61294700       ActNor.EstInrToBdy[1]

  -0.51333200       ActNor.EstInrToBdy[2]

  0.57179300         ActNor.EstInrToBdy[3]

   1061730000.000  ActNor.EstTime



  IBEX Spin Zxis (+Z S/C)

  Right Ascension - RA          154.789  deg

  Declination - DEC                10.423    deg



  IBEX Spin Axis vs. Sun Vector

  IBEX Sun Angle  -2.517     deg



  Orbit# 217 PERIGEE MPS Generated Target Vectors

  MPS Cmd Vector X             -0.892247000

  MPS Cmd Vector Y             0.418168000

  MPS Cmd Vector Z             0.170381000

    CSS Angle TLM 2.00203  CSS Sun-Pointing Angle 4.00406  24 Aug 13 @1159 CSS
Angle TLM 0.679838  CSS Sun-Pointing Angle 1.359676  28 Aug 13 @1058 *
Pre-Burn*     Thruster 1 2976 24 Aug 13 @1159 Thruster 2 2912  Thruster 3
3120  Thruster 4 3184  *Post-Burn* ** ** Thruster 1 3248 28 Aug 13
@1058 Thruster
2 3184  Thruster 3 3440  Thruster 4 3504  *Number of Pulses*    Thruster 1
272  Thruster 2 272  Thruster 3 320  Thruster 4 320  *Thruster Pairs*
** ** Thruster
1 & 2 544  Thruster 3 & 4 640
-- 
Sheral R. Wesley
SPVR., Satellite Operations
IBEX Mission OPS
(304) 279-6678
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