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 42220U 81053UL 23160.89324774 .00005655 00000-0 20883-2 0 9997
2 42220 82.9182 134.7834 0033158 119.0687 241.3828 14.32009363496529
Epoch (UTC): | 09 June 2023 21:26:16 |
Eccentricity: | 0.0033158 |
inclination: | 82.9182° |
perigee height: | 761 km |
apogee height: | 809 km |
right ascension of ascending node: | 134.7834° |
argument of perigee: | 119.0687° |
revolutions per day: | 14.32009363 |
mean anomaly at epoch: | 241.3828° |
orbit number at epoch: | 49652 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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