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 40100U 14043B 21014.57063090 -.00000182 00000-0 00000+0 0 9996
2 40100 1.0755 94.8262 0000394 5.5921 15.3391 1.00135369 7911
Epoch (UTC): | 14 January 2021 13:41:42 |
Eccentricity: | 0.0000394 |
inclination: | 1.0755° |
perigee height: | 35823 km |
apogee height: | 35826 km |
right ascension of ascending node: | 94.8262° |
argument of perigee: | 5.5921° |
revolutions per day: | 1.00135369 |
mean anomaly at epoch: | 15.3391° |
orbit number at epoch: | 791 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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