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 26094U 00004M 21016.80243082 .00000117 00000-0 52706-4 0 9995
2 26094 100.2006 335.8778 0034697 72.8847 287.6132 14.42701780 99762
Epoch (UTC): | 16 January 2021 19:15:30 |
Eccentricity: | 0.0034697 |
inclination: | 100.2006° |
perigee height: | 725 km |
apogee height: | 774 km |
right ascension of ascending node: | 335.8778° |
argument of perigee: | 72.8847° |
revolutions per day: | 14.42701780 |
mean anomaly at epoch: | 287.6132° |
orbit number at epoch: | 9976 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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