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 42418U 00055TN 22176.46045467 .00001583 00000-0 82543-3 0 9995
2 42418 98.7577 248.9821 0013527 61.0209 299.2319 14.15913586325035
Epoch (UTC): | 25 June 2022 11:03:03 |
Eccentricity: | 0.0013527 |
inclination: | 98.7577° |
perigee height: | 829 km |
apogee height: | 849 km |
right ascension of ascending node: | 248.9821° |
argument of perigee: | 61.0209° |
revolutions per day: | 14.15913586 |
mean anomaly at epoch: | 299.2319° |
orbit number at epoch: | 32503 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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