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 25394U 98043A 21016.81300604 -.00000023 00000-0 88613-5 0 9996
2 25394 98.6953 318.1424 0002392 90.8948 269.2505 14.24424753170780
Epoch (UTC): | 16 January 2021 19:30:43 |
Eccentricity: | 0.0002392 |
inclination: | 98.6953° |
perigee height: | 809 km |
apogee height: | 812 km |
right ascension of ascending node: | 318.1424° |
argument of perigee: | 90.8948° |
revolutions per day: | 14.24424753 |
mean anomaly at epoch: | 269.2505° |
orbit number at epoch: | 17078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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