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Since your mail reader does not understand this format, some or all of this message may not be legible. --B_3700616494_205460665 Content-type: text/plain; charset="UTF-8" Content-transfer-encoding: 7bit Analysis Time: 2021-04-06 22:21:25 UTC RED Threshold Updates: 0 ALL Threshold Updates: 0 Ephemeris Updates: 0 Conjunction Assessment Bodies and Types Body Name Type 1 Odyssey Active 1r Odyssey Active/Reference 2 Mars_Express Active 3 MRO Active 4 MAVEN Active 5 MOM Active 6 TGO Active 7 EMM Active 8 Phobos Natural 9 Deimos Natural 10 Viking1 Inactive 11 Viking2 Inactive 12 MGS Inactive Red (Conjunction Data < 'Red' Thresholds and Event < 14 days from Analysis Time) Bodies OXD value/limit (km) OXT value/limit (sec) CAD value/limit (km) Collision Probability CA Epoch (UTC-SCET) None All (Conjunction Data < 'All' Thresholds for <= 100 days) Bodies OXD (km) OXT (sec) CAD (km) CA Epoch (UTC-SCET) 4-6 9.2 181.5 1649.4 2021-04-11 20:59:47 4-6 9.2 181.5 576.6 2021-04-11 21:43:26 1-6 9.6 4.4 40.3 2021-04-17 18:23:46 1-6 9.6 4.4 10.5 2021-04-17 19:22:58 1-6 9.5 38.0 19.0 2021-04-17 20:22:02 1-6 9.5 38.0 36.8 2021-04-17 21:21:14 1-4 -3.0 1013.7 551.6 2021-05-09 05:52:48 1-4 6.2 2240.8 979.4 2021-05-09 09:38:28 Notes OXD means "Orbit Crossing Distance". OXT means "Orbit Crossing Timing". CAD means "Close Approach Distance". Data for active spacecraft and natural bodies are displayed in the tables above. Data for inactive spacecraft are not displayed, but they are available in the conjunction metric tables and plots, which have been stored in the output directory listed below. Data for reference trajectories are not considered for Red events, but are considered in the All section for events not covered by the predicts file. Reference trajectories use the same thresholds as the nominal trajectories. The note after the probability value listed for RED events refers to the source of covariance data used for the probability calculation, with the following definitions: C - Covariance data provided by the mission in OEM format. P - A covariance converted from the RED threshold polynomial coefficients listed below. N - No covariance data, worst case covariance assumed for this body. No Data - Probability could not be calculated due to a lack of covariance data from both bodies. For more information, please see the point of contact listed below. Analysis time: 2021-04-06 22:21:25 UTC Active spacecraft: Odyssey, Mars Express, MRO, MAVEN, MOM, TGO, EMM Natural bodies: Phobos, Deimos Inactive spacecraft: Viking1, Viking2, MGS Output directory: /nav/home/jplmdnav/MADCAP/Mars/archive Point of contact: MADCAP_Mars@jpl.nasa.gov MADCAP build: 3.1.2 Red Thresholds -- Polynomial Coefficients Body Name OXD0 (km) OXD1 (km/t) OXD2 (km/t^2) OXT0 (sec) OXT1 (sec/t) OXT2 (sec/t^2) 1 Odyssey 0.0050 0.0013 0.0000 0.0705 -0.0411 0.0096 2 Mars_Express 1.0000 0.0000 0.0000 10.0000 0.0000 0.0000 3 MRO 0.0877 -0.0315 0.0040 0.0100 0.4939 0.0765 4 MAVEN 0.5000 0.1000 0.0030 2.1000 0.4000 0.3300 5 MOM 0.2498 0.0014 0.0012 0.0100 33.0089 0.3246 6 TGO 1.0000 0.0000 0.0000 10.0000 0.0000 0.0000 7 EMM 1.0000 0.0000 0.0000 10.0000 0.0000 0.0000 8 Phobos 30.0000 0.0000 0.0000 15.0000 0.0000 0.0000 9 Deimos 40.0000 0.0000 0.0000 20.0000 0.0000 0.0000 Red OX Distance Threshold = OXD0 + (OXD1 * t) + (OXD2 * t^2) [km] Red OX Timing Threshold = OXT0 + (OXT1 * t) + (OXT2 * t^2) [sec] where t = CA Epoch - Ephemeris File Submit Time (in days) Red thresholds are based on 3-sigma values. Thresholds listed as "P" are based on a quadratic fit of the 3-sigma values as a function of time to the event. The polynomial coefficients used are listed in the table above. Lines for coefficients which have been updated since the last run are colored blue, and each line's body is marked with an "*". Thresholds listed as "C" are based on 3-sigma covariance data provided by the mission. All Thresholds -- Constants Body Name OXD (km) CAD (km) 1 Odyssey 10 100 2 Mars_Express 10 100 3 MRO 10 300 4 MAVEN 10 3000 5 MOM 20 100 6 TGO 10 100 7 EMM 10 100 8 Phobos 45 100 9 Deimos 60 200 All OX Distance Threshold = OXD All CA Distance Threshold = CAD All thresholds are always constants. The constants used are listed in the table above. Lines for constants which have been updated since the last run are colored blue, and each line's body is marked with an "*". Ephemerides Body Ephemeris Submitted Begin End 1 p_m_od85638-85643_87123_v1.bsp 2021-04-05 23:26:25 UTC 04-APR-2021 17:03:50 UTC 04-AUG-2021 23:58:50 UTC 1r p_m_od85470-85472_86783_v1.bsp_V0.1 Analysis Time 21-MAR-2021 21:30:50 UTC 07-JUL-2021 23:58:50 UTC 2 MOEM_210329OAS_PREDICT__0001.CR.bsp 2021-03-29 10:18:32 UTC 18-MAR-2021 21:43:09 UTC 27-APR-2021 16:50:31 UTC 3 pf_psp_rec68817_68812_69588_p-v1.bsp 2021-04-01 16:20:06 UTC 01-APR-2021 04:03:50 UTC 31-MAY-2021 14:43:50 UTC 4 trj_orb_13694-13696_13949_v1_mvn.bsp 2021-04-05 16:20:26 UTC 04-APR-2021 20:08:50 UTC 13-MAY-2021 06:03:50 UTC 5 ISRO-MOM-2021-03-24-OD2708-096-v1.xsp.bsp 2021-04-06 10:33:15 UTC 24-MAR-2021 00:00:00 UTC 29-APR-2021 00:10:00 UTC 6 TOEM_210329OAS_PREDICT__0001.CR.bsp 2021-03-29 13:24:25 UTC 26-FEB-2021 23:58:50 UTC 08-MAY-2021 15:22:52 UTC 7 62_pred_20210330_20210709_od038_noburn_v1.xsp.bsp 2021-03-31 23:53:21 UTC 30-MAR-2021 15:33:50 UTC 09-JUL-2021 00:00:50 UTC 8 mar097.2010-2029.bsp Analysis Time 29-DEC-2009 23:58:53 UTC 01-JAN-2030 23:58:50 UTC 9 mar097.2010-2029.bsp Analysis Time 29-DEC-2009 23:58:53 UTC 01-JAN-2030 23:58:50 UTC 10 Viking1_210101_220101.boa Analysis Time 01-JAN-2021 11:58:50 UTC 01-JAN-2022 11:58:50 UTC 11 viking2_210101_220101.boa Analysis Time 01-JAN-2021 11:58:50 UTC 01-JAN-2022 11:58:50 UTC 12 p_201029-211029-061215_10yr_nominal.nio Analysis Time 29-OCT-2020 05:28:50 UTC 29-OCT-2021 06:28:50 UTC Ephemeris files for the bodies analyzed are listed in the table above. Lines for files which have been updated since the last run are colored blue, and each line's body is marked with an "*". --B_3700616494_205460665 Content-type: text/html; charset="UTF-8" Content-transfer-encoding: quoted-printable

Analysis Time: 2021-04-06 22:21:25 UTC=

RED Threshold Updates: 0
ALL Threshold Updates: 0
Ephemeris Updates: 0

Conjunction Assessment Bodies and Types

Body Name Type
1 Odyssey Active
1r Odyssey Active/Reference
2 Mars_Express Active
3 MRO Active
4 MAVEN Active
5 MOM Active
6 TGO Active
7 EMM Active
8 Phobos Natural
9 Deimos Natural
10 Viking1 Inactive
11 Viking2 Inactive
12 MGS Inactive

Red (Conjunction Data < 'Red' Thre= sholds and Event < 14 days from Analysis Time)

<= col style=3D"width: 3em">
Bodies OXD value/limit (km) OXT value/limit (sec) CAD value/limit (km) Collision Probability CA Epoch (UTC-SCET)
None

All (Conjunction Data < 'All' Thresholds for &= lt;=3D 100 days)

Bodies OXD (km) OXT (sec) CAD (km) CA Epoch (UTC-SCET)
4-6 9.2 181.5 1649.4 2021-04-11 20:59:47
4-6 9.2 181.5 576.6 2021-04-11 21:43:26
1-6 9.6 4.4 40.3 2021-04-17 18:23:46
1-6 9.6 4.4 10.5 2021-04-17 19:22:58
1-6 9.5 38.0 19.0 2021-04-17 20:22:02
1-6 9.5 38.0 36.8 2021-04-17 21:21:14
1-4 -3.0 1013.7 551.6 2021-05-09 05:52:48
1-4 6.2 2240.8 979.4 2021-05-09 09:38:28

Notes

OXD means "Orbit Crossing Distance". OXT means "Orbit Cro= ssing Timing". CAD means "Close Approach Distance".

Data for active spacecraft and natural bodies are displayed in the table= s above. Data for inactive spacecraft are not displayed, but they are availa= ble in the conjunction metric tables and plots, which have been stored in th= e output directory listed below. Data for reference trajectories are not considered for Red events, but are= considered in the All section for events not covered by the predicts file. = Reference trajectories use the same thresholds as the nominal trajectories.

The note after the probability value listed for RED events refers to the= source of covariance data used for the probability calculation, with the fo= llowing definitions:

C - Covariance data provided by the mission in OEM format.
P - A covariance converted from the RED threshold polynomial coefficients l= isted below.
N - No covariance data, worst case covariance assumed for this body.
No Data - Probability could not be calculated due to a lack of covariance d= ata from both bodies.

For more information, please see the point of contact listed below.

Analysis time: 2021-04-06 22:21:25 UTC
Active spacecraft: Odyssey, Mars Express, MRO, MAVEN, MOM, TGO, EMM
Natural bodies: Phobos, Deimos
Inactive spacecraft: Viking1, Viking2, MGS
Output directory: /nav/home/jplmdnav/MADCAP/Mars/archive
Point of contact: MADCAP_Mars@jpl.nasa.gov
MADCAP build: 3.1.2

Red Thresholds -- Polynomial Coefficients<= /b>

Body Name OXD0 (km) OXD1 (km/t) OXD2 (km/t^2) OXT0 (sec) OXT1 (sec/t) OXT2 (sec/t^2)
1 Odyssey 0.0050 0.0013 0.0000 0.0705 -0.0411 0.0096
2 Mars_Express 1.0000 0.0000 0.0000 10.0000 0.0000 0.0000
3 MRO 0.0877 -0.0315 0.0040 0.0100 0.4939 0.0765
4 MAVEN 0.5000 0.1000 0.0030 2.1000 0.4000 0.3300
5 MOM 0.2498 0.0014 0.0012 0.0100 33.0089 0.3246
6 TGO 1.0000 0.0000 0.0000 10.0000 0.0000 0.0000
7 EMM 1.0000 0.0000 0.0000 10.0000 0.0000 0.0000
8 Phobos 30.0000 0.0000 0.0000 15.0000 0.0000 0.0000
9 Deimos 40.0000 0.0000 0.0000 20.0000 0.0000 0.0000

Red OX Distance Threshold =3D OXD0 + (OXD1 * t) + (OXD2 * t^2) [km= ]
Red OX Timing Threshold =3D OXT0 + (OXT1 * t) + (OXT2 * t^2) [sec] where t =3D CA Epoch - Ephemeris File Submit Time (in days)

Red thresholds are based on 3-sigma values. Thresholds listed as "P= " are based on a quadratic fit of the 3-sigma values as a function of t= ime to the event. The polynomial coefficients used are listed in the table a= bove. Lines for coefficients which have been updated since the last run are colored blue, and each line's body is = marked with an "*". Thresholds listed as "C" are based o= n 3-sigma covariance data provided by the mission.

All Thresholds -- Constants

Body Name OXD (km) CAD (km)
1 Odyssey 10 100
2 Mars_Express 10 100
3 MRO 10 300
4 MAVEN 10 3000
5 MOM 20 100
6 TGO 10 100
7 EMM 10 100
8 Phobos 45 100
9 Deimos 60 200

All OX Distance Threshold =3D OXD
All CA Distance Threshold =3D CAD

All thresholds are always constants. The constants used are listed in th= e table above. Lines for constants which have been updated since the last ru= n are colored blue, and each line's body is marked with an "*".

Ephemerides

Body Ephemeris Submitted Begin End
1 p_m_od85638-85643_87123_v1.bsp 2021-04-05 23:26:25 UTC 04-APR-2021 17:03:50 UTC 04-AUG-2021 23:58:50 UTC
1r p_m_od85470-85472_86783_v1.bsp_V0.1 Analysis Time 21-MAR-2021 21:30:50 UTC 07-JUL-2021 23:58:50 UTC
2 MOEM_210329OAS_PREDICT__0001.CR.bsp 2021-03-29 10:18:32 UTC 18-MAR-2021 21:43:09 UTC 27-APR-2021 16:50:31 UTC
3 pf_psp_rec68817_68812_69588_p-v1.bsp 2021-04-01 16:20:06 UTC 01-APR-2021 04:03:50 UTC 31-MAY-2021 14:43:50 UTC
4 trj_orb_13694-13696_13949_v1_mvn.bsp 2021-04-05 16:20:26 UTC 04-APR-2021 20:08:50 UTC 13-MAY-2021 06:03:50 UTC
5 ISRO-MOM-2021-03-24-OD2708-096-v1.xsp.bsp 2021-04-06 10:33:15 UTC 24-MAR-2021 00:00:00 UTC 29-APR-2021 00:10:00 UTC
6 TOEM_210329OAS_PREDICT__0001.CR.bsp 2021-03-29 13:24:25 UTC 26-FEB-2021 23:58:50 UTC 08-MAY-2021 15:22:52 UTC
7 62_pred_20210330_20210709_od038_noburn_v1.xsp.b= sp 2021-03-31 23:53:21 UTC 30-MAR-2021 15:33:50 UTC 09-JUL-2021 00:00:50 UTC
8 mar097.2010-2029.bsp Analysis Time 29-DEC-2009 23:58:53 UTC 01-JAN-2030 23:58:50 UTC
9 mar097.2010-2029.bsp Analysis Time 29-DEC-2009 23:58:53 UTC 01-JAN-2030 23:58:50 UTC
10 Viking1_210101_220101.boa Analysis Time 01-JAN-2021 11:58:50 UTC 01-JAN-2022 11:58:50 UTC
11 viking2_210101_220101.boa Analysis Time 01-JAN-2021 11:58:50 UTC 01-JAN-2022 11:58:50 UTC
12 p_201029-211029-061215_10yr_nominal.nio Analysis Time 29-OCT-2020 05:28:50 UTC 29-OCT-2021 06:28:50 UTC

Ephemeris files for the bodies analyzed are listed in the table above. L= ines for files which have been updated since the last run are colored blue, = and each line's body is marked with an "*".

--B_3700616494_205460665--