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 17291U 87001B 22139.49734955 .00000084 00000-0 61440-4 0 9990
2 17291 82.4700 217.3912 0012149 49.9419 310.2805 13.84594147787389
Epoch (UTC): | 19 May 2022 11:56:11 |
Eccentricity: | 0.0012149 |
inclination: | 82.4700° |
perigee height: | 939 km |
apogee height: | 956 km |
right ascension of ascending node: | 217.3912° |
argument of perigee: | 49.9419° |
revolutions per day: | 13.84594147 |
mean anomaly at epoch: | 310.2805° |
orbit number at epoch: | 78738 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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