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 20303U 89085B 22145.67487545 .00016221 00000-0 42051-3 0 9995
2 20303 35.6383 232.7260 0080241 6.7344 353.4447 15.34893598776958
Epoch (UTC): | 25 May 2022 16:11:49 |
Eccentricity: | 0.0080241 |
inclination: | 35.6383° |
perigee height: | 406 km |
apogee height: | 516 km |
right ascension of ascending node: | 232.7260° |
argument of perigee: | 6.7344° |
revolutions per day: | 15.34893598 |
mean anomaly at epoch: | 353.4447° |
orbit number at epoch: | 77695 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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