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 23605U 95033A 22224.09712966 0.00000601 00000-0 58587-4 0 05
2 23605 98.1934 9.6386 0022665 337.2186 22.4725 14.92337956 06
Epoch (UTC): | 12 August 2022 02:19:52 |
Eccentricity: | 0.0022665 |
inclination: | 98.1934° |
perigee height: | 575 km |
apogee height: | 606 km |
right ascension of ascending node: | 9.6386° |
argument of perigee: | 337.2186° |
revolutions per day: | 14.92337956 |
mean anomaly at epoch: | 22.4725° |
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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