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 45873U 20046A 22226.88716678 0.00010523 00000-0 70031-3 0 02
2 45873 53.9758 218.1394 0006906 167.5761 192.4238 15.06654341 02
Epoch (UTC): | 14 August 2022 21:17:31 |
Eccentricity: | 0.0006906 |
inclination: | 53.9758° |
perigee height: | 541 km |
apogee height: | 551 km |
right ascension of ascending node: | 218.1394° |
argument of perigee: | 167.5761° |
revolutions per day: | 15.06654341 |
mean anomaly at epoch: | 192.4238° |
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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