View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 35685U 09041E 21016.12846389 .00000055 00000-0 13469-4 0 9999
2 35685 98.2384 59.5210 0059581 137.8681 222.7135 14.84367646620422
Epoch (UTC): | 16 January 2021 03:04:59 |
Eccentricity: | 0.0059581 |
inclination: | 98.2384° |
perigee height: | 574 km |
apogee height: | 657 km |
right ascension of ascending node: | 59.5210° |
argument of perigee: | 137.8681° |
revolutions per day: | 14.84367646 |
mean anomaly at epoch: | 222.7135° |
orbit number at epoch: | 62042 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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