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 24257.15110111 .00030841 00000-0 16430-2 0 9990
2 22 50.2791 351.6161 0106851 91.6529 269.6667 15.10065523457642
Epoch (UTC): | 13 September 2024 03:37:35 |
Eccentricity: | 0.0106851 |
inclination: | 50.2791° |
perigee height: | 462 km |
apogee height: | 610 km |
right ascension of ascending node: | 351.6161° |
argument of perigee: | 91.6529° |
revolutions per day: | 15.10065523 |
mean anomaly at epoch: | 269.6667° |
orbit number at epoch: | 45764 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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