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 22229.92779446 .00016904 00000-0 41700-3 0 9998
2 20303 35.6385 56.7007 0077240 44.7617 315.9313 15.36602915789371
Epoch (UTC): | 17 August 2022 22:16:01 |
Eccentricity: | 0.0077240 |
inclination: | 35.6385° |
perigee height: | 403 km |
apogee height: | 509 km |
right ascension of ascending node: | 56.7007° |
argument of perigee: | 44.7617° |
revolutions per day: | 15.36602915 |
mean anomaly at epoch: | 315.9313° |
orbit number at epoch: | 78937 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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