Main mission events

The following tables show the main mission events.
R: s/c radius vector (millions of kilometers); h: altitude above the Sun surface (millions of kilometers); hrsun: altitude above the Sun (solar radii); V: s/c heliocentric speed (m/s); Lh: s/c heliocentric longitude (degrees).

# UTC time R h hrsun V Lh ECC or T
P12018-11-06 03:27:5124.8224.1234.795328150.1
A12019-01-20 01:04:04140.34139.64200.616859-29.90.699453
P22019-04-04 22:39:5624.8224.1234.795327150.1149.80
A22019-06-18 20:15:33140.34139.64200.616859-29.90.699449
P32019-09-01 17:50:1824.8224.1234.795330150.1149.80
A32019-11-15 15:25:09140.34139.64200.616858-29.90.699462
P42020-01-29 09:37:4219.3918.7026.9109179157.2149.66
A42020-04-03 09:00:44130.83130.13187.016183-22.80.741816
P52020-06-07 08:23:0419.3918.7026.9109181157.2129.95
A52020-08-02 05:04:07122.17121.48174.515021-29.60.726037
P62020-09-27 09:16:0214.1613.4619.3129609150.4112.04
A62020-11-22 13:27:53122.17121.48174.515021-29.60.792283
P72021-01-17 17:39:1814.1613.4619.3129611150.4112.35
A72021-03-09 03:37:07117.07116.38167.214020-33.90.784213
P82021-04-29 08:46:5211.1110.4215.0147686146.1101.63
A82021-06-19 13:58:46117.07116.38167.214020-33.90.826598
P92021-08-09 19:10:3311.1110.4215.0147686146.1102.43
A92021-09-30 00:21:33117.07116.38167.214020-33.90.826597
P102021-11-21 08:25:249.248.5412.3163018149.0103.55
A102022-01-08 12:00:35113.78113.08162.513235-31.00.849815
P112022-02-25 15:35:529.248.5412.3163018149.096.30
A112022-04-14 19:12:55113.78113.09162.513235-31.00.849818
P122022-06-01 22:50:079.248.5412.3163013149.096.30
A122022-07-20 02:26:46113.78113.09162.513236-31.00.849809
P132022-09-06 06:03:359.248.5412.3163014149.096.30
A132022-10-24 09:39:30113.78113.08162.513236-31.00.849809
P142022-12-11 13:15:489.248.5412.3163008149.096.30
A142023-01-28 16:52:57113.78113.09162.513236-31.00.849801
P152023-03-17 20:30:349.248.5412.3162999149.096.30
A152023-05-05 00:08:07113.78113.09162.513237-31.00.849786
P162023-06-22 03:45:549.248.5412.3162994149.096.30
A162023-08-09 07:23:34113.78113.08162.513236-31.00.849778
P172023-09-27 23:28:267.967.2610.4176463151.397.82
A172023-11-13 00:11:44111.43110.73159.112599-28.70.866718
P182023-12-29 00:55:067.967.2610.4176464151.392.06
A182024-02-13 01:39:30111.43110.73159.112599-28.70.866719
P192024-03-30 02:22:487.967.2610.4176464151.392.06
A192024-05-15 03:05:57111.43110.73159.112599-28.70.866719
P202024-06-30 03:49:087.967.2610.4176464151.392.06
A202024-08-15 04:33:14111.43110.73159.112599-28.70.866720
P212024-09-30 05:17:157.967.2610.4176467151.392.06
A212024-11-10 06:29:47109.38108.68156.111968-31.50.864395
P222024-12-24 11:52:206.866.178.9190771148.585.27
A222025-02-06 17:16:03109.38108.68156.211970-31.50.881923
P232025-03-22 22:39:466.866.178.9190771148.588.45
A232025-05-06 04:03:37109.38108.68156.211970-31.50.881923
P242025-06-19 09:27:236.866.178.9190771148.588.45
A242025-08-02 14:51:57109.38108.68156.211969-31.50.881924
Here are the s/c apsides. Pi is the i-th perihelion, Ai is the i-th aphelion.
The eccentricity (ECC) is calculated as e= (Ai - Pi) / (Ai + Pi).
The orbital period (T, days) is calculated as the time between two consecutive perihelia.
# UTC time R V Lh
A12018-11-02 16:45:4330.498425890.1
D12018-11-21 12:32:2468.4247668-89.9
A22019-04-01 11:55:0630.498424890.1
D22019-04-20 07:32:0168.3947683-89.9
A32019-08-29 07:05:5030.498425190.1
D32019-09-17 02:41:1668.3947684-89.9
A42020-09-25 09:03:5120.1110607376.4
D42020-10-02 08:04:1834.3875978-103.6
A52021-01-15 17:27:0920.1110607376.4
D52021-01-22 16:26:5334.3875981-103.6
A62023-09-27 02:56:3611.6314350176.6
D62023-09-30 02:44:1920.53103467-103.4
A72023-12-28 04:23:4011.6314351476.7
D72023-12-31 04:12:0720.54103450-103.3
A82024-03-29 05:50:0711.6414347576.6
D82024-04-01 05:35:5420.52103506-103.4
A92024-06-29 07:16:2611.6414347476.6
D92024-07-02 07:02:1420.52103506-103.4
A102024-09-29 08:44:2211.6414346976.6
D102024-10-02 08:29:2420.51103519-103.4
Here are the orbital nodes. Ai is the i-th ascending node, Di is the i-th descending node. The reference plane is the mean ecliptic of J2000.