Analysis Time: 2026-04-28 20:45:26 UTC

RED Threshold Updates: 0
ALL Threshold Updates: 0
Ephemeris Updates: 1
Failed Pair: (Odyssey, TGO), (MRO, TGO), (TGO, EMM), (TGO, Psyche), (TGO, Phobos), (TGO, Deimos), (TGO, Mariner 9), (TGO, Viking1), (TGO, Viking2), (TGO, MGS), (TGO, MOM), (TGO, MAVEN)

Conjunction Assessment Bodies and Types

Body Name Type
1 Odyssey Active
2 Mars_Express Active
3 MRO Active
4 TGO Active
5 EMM Active
6 Tianwen1 Active
7 Psyche Active
8 Phobos Natural
9 Deimos Natural
10 Mariner_9 Inactive
11 Viking1 Inactive
12 Viking2 Inactive
13 MGS Inactive
14 MOM Inactive
15 MAVEN 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)
1-2 9.16 53.90 78.47 2026-05-17 12:53:48

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: 2026-04-28 20:45:26 UTC
Active spacecraft: Odyssey, Mars Express, MRO, TGO, EMM, Tianwen1, Psyche
Natural bodies: Phobos, Deimos
Inactive spacecraft: Mariner 9, Viking1, Viking2, MGS, MOM, MAVEN
Output directory: /nav/home/jplmdnav/MADCAP/Mars/archive
Point of contact: MADCAP_Mars@jpl.nasa.gov
MADCAP build: 4.0
Monte Version: 172.1

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 0.1500
4 TGO 1.0000 0.0000 0.0000 10.0000 0.0000 0.0000
5 EMM 1.0000 0.0000 0.0000 10.0000 0.0000 0.0000
6 Tianwen1 1.0000 0.0000 0.0000 10.0000 0.0000 0.0000
7 Psyche 5.0000 0.0000 0.0000 10.0000 0.0000 0.0000
8 Phobos 20.0000 0.0000 0.0000 20.0000 0.0000 0.0000
9 Deimos 15.0000 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 10.00 100.00
2 Mars_Express 10.00 100.00
3 MRO 10.00 300.00
4 TGO 10.00 100.00
5 EMM 10.00 100.00
6 Tianwen1 10.00 100.00
7 Psyche 30.00 100.00
8 Phobos 45.00 100.00
9 Deimos 60.00 200.00

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_od108089-108094_109567_v1.bsp 2026-04-27 23:10:53 UTC 27-APR-2026 08:26:50 UTC 26-AUG-2026 23:58:50 UTC
2 MOEM_260427OAS_PREDICT__0001.CR.bsp 2026-04-27 14:23:41 UTC 01-APR-2026 23:53:43 UTC 24-MAY-2026 05:33:22 UTC
3 pf_psp_rec92530_92525_93300_p-v1.bsp 2026-04-23 15:55:14 UTC 22-APR-2026 21:43:50 UTC 22-JUN-2026 08:08:50 UTC
4 TOEM_260427OAS_PREDICT__0001.CR.bsp 2026-04-27 12:29:51 UTC 16-APR-2026 23:48:04 UTC 06-JUN-2026 15:07:52 UTC
5 62_pred_20260403_20260901_od194_v1.xsp.bsp 2026-04-06 21:24:23 UTC 03-APR-2026 06:13:50 UTC 01-SEP-2026 00:00:50 UTC
6 CCSDS_OEM_CM1_20260313000459_0001.bsp Analysis Time 13-MAR-2026 00:00:30 UTC 03-APR-2026 00:00:00 UTC
7 psyche_sps_251114-260801_260421_v1.bsp 2026-04-22 04:32:18 UTC 14-NOV-2025 23:58:50 UTC 01-AUG-2026 12:00:00 UTC
8 mar099_2026_2030.bsp Analysis Time 01-JAN-2026 12:00:00 UTC 01-JAN-2030 12:00:00 UTC
9 mar099_2026_2030.bsp Analysis Time 01-JAN-2026 12:00:00 UTC 01-JAN-2030 12:00:00 UTC
10 Mariner9_260101_270101.boa Analysis Time 01-JAN-2026 12:00:00 UTC 01-JAN-2027 12:00:00 UTC
11 Viking1_260101_270101.boa Analysis Time 01-JAN-2026 12:00:00 UTC 01-JAN-2027 12:00:00 UTC
12 Viking2_260101_270101.boa Analysis Time 01-JAN-2026 12:00:00 UTC 01-JAN-2027 12:00:00 UTC
13 p_251103-261103-061219_10yr_nominal.nio Analysis Time 03-NOV-2025 05:28:50 UTC 03-NOV-2026 06:28:50 UTC
14 JPL_MOM_260101-270101.bsp Analysis Time 01-JAN-2026 12:00:00 UTC 01-JAN-2027 12:00:00 UTC
15 trj_orb_24945-24946_26709_v2stoch4min-0451_v1_mvn.bsp 2026-01-27 00:16:50 UTC 06-DEC-2025 00:26:50 UTC 01-SEP-2026 00:58:50 UTC

Ephemeris files for the bodies analyzed are listed in the table above. Files colored red have been expired. Files colored blue have been updated since the last run. Each line's body is marked with an "*".