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 26069U 00006A 21019.50464063 -.00000292 00000-0 -13010-3 0 9993
2 26069 70.9934 129.8491 0009457 31.3799 328.7885 14.13424185 81540
Epoch (UTC): | 19 January 2021 12:06:40 |
Eccentricity: | 0.0009457 |
inclination: | 70.9934° |
perigee height: | 841 km |
apogee height: | 854 km |
right ascension of ascending node: | 129.8491° |
argument of perigee: | 31.3799° |
revolutions per day: | 14.13424185 |
mean anomaly at epoch: | 328.7885° |
orbit number at epoch: | 8154 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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