IBEX_2022_264_o0582a_v001.scr,

and I approve.

The only constraint violations in

IBEX_2022_264_o0582a_v001.ccvr

are from the removal of the

ACT_SetSpinPulseProtectEnable Enable

commands (2) and the proximity of two contacts; the violations are expected.

Ascending and descending command sequences are consistent with each other, 15 Re ascending, the apogee maneuver time and 15 Re descending as determined from the OEF,

IBEX_2022_264_o0582a_v001.oef,

and as verified with ibex_orbit.

There are no star tracker outages.

The ground station command sequences are correct and the timing and bit rates match those in the contacts file,

IBEX_Orbit582_Contacts.txt,

for all contacts (4).

We are doing battery cell balancing and the balancing commands are correct and offset by enough time from other commands.

The inertial precession maneuver at perigee of orbit 581 leaves us pointing in safe directions for the orbit 582 arc A ascending and descending sequences:

ibex_rotate -o -u -0.997725,0.06487,0.018325 -w ibex-sun -t 2022/09:22:05:40:16

Quaternion +0.000000,+0.000000,+0.000000,+0.000000

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.997725,+0.064870,+0.018325

which is R.A. +176.280 Decl. +1.050

missing R.A. +179.016 Decl. +0.410 (ibex-sun)

error is R.A. +2.736 Decl. +0.640

for a total 2.810 deg

ibex_rotate -o -u -0.997725,0.06487,0.018325 -w ibex-sun -t 2022/09:26:01:42:36

Quaternion +0.000000,+0.000000,+0.000000,+0.000000

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.997725,+0.064870,+0.018325

which is R.A. +176.280 Decl. +1.050

missing R.A. +182.354 Decl. -1.014 (ibex-sun)

error is R.A. +6.074 Decl. +2.064

for a total 6.414 deg

The inertial precession maneuver at apogee leaves us pointing in safe directions at the time of the maneuver and for arc B ascending and descending sequences:

ibex_rotate -o -u -0.999868,-0.007818,-0.014276 -w ibex-sun -t 2022/09:26:03:25:44

Quaternion +0.000000,+0.000000,+0.000000,+0.000000

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.999868,-0.007818,-0.014276

which is R.A. +180.448 Decl. -0.818

missing R.A. +182.418 Decl. -1.040 (ibex-sun)

error is R.A. +1.970 Decl. +0.222

for a total 1.982 deg

ibex_rotate -o -u -0.999868,-0.007818,-0.014276 -w ibex-sun -t 2022/09:26:05:00:50

Quaternion +0.000000,+0.000000,+0.000000,+0.000000

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.999868,-0.007818,-0.014276

which is R.A. +180.448 Decl. -0.818

missing R.A. +182.477 Decl. -1.065 (ibex-sun)

error is R.A. +2.029 Decl. +0.247

for a total 2.044 deg

ibex_rotate -o -u -0.999868,-0.007818,-0.014276 -w ibex-sun -t 2022/09:30:19:05:19

Quaternion +0.000000,+0.000000,+0.000000,+0.000000

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.999868,-0.007818,-0.014276

which is R.A. +180.448 Decl. -0.818

missing R.A. +186.716 Decl. -2.890 (ibex-sun)

error is R.A. +6.268 Decl. +2.072

for a total 6.598 deg

The inertial precession maneuver at perigee leaves us pointing in safe directions at the time of the maneuver and at orbit 583 apogee:

ibex_rotate -o -u -0.99583,-0.07972,-0.044352 -w ibex-sun -t 2022/09:30:23:16:33

Quaternion +0.000000,+0.000000,+0.000000,+0.000000

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.995830,-0.079720,-0.044352

which is R.A. +184.577 Decl. -2.542

missing R.A. +186.880 Decl. -2.968 (ibex-sun)

error is R.A. +2.303 Decl. +0.426

for a total 2.339 deg

ibex_rotate -o -u -0.99583,-0.07972,-0.044352 -w ibex-sun -t 2022-10-05T18:33:05.296Z

Quaternion +0.000000,+0.000000,+0.000000,+0.000000

points axis +1.000000,+0.000000,+0.000000

towards ECI -0.995830,-0.079720,-0.044352

which is R.A. +184.577 Decl. -2.542

missing R.A. +191.134 Decl. -4.773 (ibex-sun)

error is R.A. +6.557 Decl. +2.231

for a total 6.913 deg

Lo Normal mode for the entire orbit.

There is no overlap with orbit 581 commands by manual inspection or by checking at

http://ibex.unh.edu/cgi-bin/ats.cgi.

Command Approval Checklist is attached.

Ken