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 22138.80654044 0.00000000 00000-0 00000-0 0 04
2 45606 45.0286 59.2282 0009459 137.5185 222.4810 15.78192232 02
Epoch (UTC): | 18 May 2022 19:21:25 |
Eccentricity: | 0.0009459 |
inclination: | 45.0286° |
perigee height: | 329 km |
apogee height: | 342 km |
right ascension of ascending node: | 59.2282° |
argument of perigee: | 137.5185° |
revolutions per day: | 15.78192232 |
mean anomaly at epoch: | 222.4810° |
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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