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 59U 60013B 21023.05014719 .00000088 00000-0 13278-5 0 9991
2 59 28.2476 170.1816 0189280 329.3075 29.6517 13.52982355976876
Epoch (UTC): | 23 January 2021 01:12:12 |
Eccentricity: | 0.0189280 |
inclination: | 28.2476° |
perigee height: | 920 km |
apogee height: | 1202 km |
right ascension of ascending node: | 170.1816° |
argument of perigee: | 329.3075° |
revolutions per day: | 13.52982355 |
mean anomaly at epoch: | 29.6517° |
orbit number at epoch: | 97687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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