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 45606U 20029A 22208.68361964 0.00000000 00000-0 00000-0 0 04
2 45606 45.0145 7.9433 0010612 202.4342 157.5653 15.78183095 04
Epoch (UTC): | 27 July 2022 16:24:24 |
Eccentricity: | 0.0010612 |
inclination: | 45.0145° |
perigee height: | 328 km |
apogee height: | 343 km |
right ascension of ascending node: | 7.9433° |
argument of perigee: | 202.4342° |
revolutions per day: | 15.78183095 |
mean anomaly at epoch: | 157.5653° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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