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 58U 60013A 22176.50932143 .00000092 00000-0 15202-4 0 9993
2 58 28.3282 310.2588 0164999 59.7026 301.9734 13.46335449 38688
Epoch (UTC): | 25 June 2022 12:13:25 |
Eccentricity: | 0.0164999 |
inclination: | 28.3282° |
perigee height: | 962 km |
apogee height: | 1209 km |
right ascension of ascending node: | 310.2588° |
argument of perigee: | 59.7026° |
revolutions per day: | 13.46335449 |
mean anomaly at epoch: | 301.9734° |
orbit number at epoch: | 3868 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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