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 22U 59009A 25168.17616784 .00008805 00000-0 38352-3 0 9994
2 22 50.2719 91.2229 0091870 103.5888 257.5322 15.19204735499648
Epoch (UTC): | 17 June 2025 04:13:40 |
Eccentricity: | 0.0091870 |
inclination: | 50.2719° |
perigee height: | 445 km |
apogee height: | 571 km |
right ascension of ascending node: | 91.2229° |
argument of perigee: | 103.5888° |
revolutions per day: | 15.19204735 |
mean anomaly at epoch: | 257.5322° |
orbit number at epoch: | 49964 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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