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 22913U 93073C 24281.19005688 .00224253 -24932-5 31941-2 0 9997
2 22913 6.7472 189.7063 2560875 315.1556 26.7773 10.36667354641923
Epoch (UTC): | 07 October 2024 04:33:40 |
Eccentricity: | 0.2560875 |
inclination: | 6.7472° |
perigee height: | 231 km |
apogee height: | 4782 km |
right ascension of ascending node: | 189.7063° |
argument of perigee: | 315.1556° |
revolutions per day: | 10.36667354 |
mean anomaly at epoch: | 26.7773° |
orbit number at epoch: | 64192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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