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 36089U 09061B 22227.40304071 .00000201 00000-0 61392-4 0 9994
2 36089 98.2599 191.7215 0082072 13.2101 137.7794 14.50014277674773
Epoch (UTC): | 15 August 2022 09:40:22 |
Eccentricity: | 0.0082072 |
inclination: | 98.2599° |
perigee height: | 667 km |
apogee height: | 784 km |
right ascension of ascending node: | 191.7215° |
argument of perigee: | 13.2101° |
revolutions per day: | 14.50014277 |
mean anomaly at epoch: | 137.7794° |
orbit number at epoch: | 67477 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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