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 25544U 98067A 22229.72706019 .00005526 00000-0 10397-3 0 9990
2 25544 51.6430 31.7146 0005515 132.1754 69.1269 15.50212612354721
Epoch (UTC): | 17 August 2022 17:26:58 |
Eccentricity: | 0.0005515 |
inclination: | 51.6430° |
perigee height: | 412 km |
apogee height: | 420 km |
right ascension of ascending node: | 31.7146° |
argument of perigee: | 132.1754° |
revolutions per day: | 15.50212612 |
mean anomaly at epoch: | 69.1269° |
orbit number at epoch: | 35472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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