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 25407U 98045B 21063.40703465 .00000238 00000-0 14512-3 0 9994
2 25407 71.0105 71.2711 0009599 290.5616 69.4477 14.15835699168142
Epoch (UTC): | 04 March 2021 09:46:07 |
Eccentricity: | 0.0009599 |
inclination: | 71.0105° |
perigee height: | 832 km |
apogee height: | 846 km |
right ascension of ascending node: | 71.2711° |
argument of perigee: | 290.5616° |
revolutions per day: | 14.15835699 |
mean anomaly at epoch: | 69.4477° |
orbit number at epoch: | 16814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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