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 41273U 00055FZ 22226.19557250 .00003168 00000-0 11479-2 0 9997
2 41273 98.9403 17.7932 0064795 188.3336 171.6776 14.32960510346799
Epoch (UTC): | 14 August 2022 04:41:37 |
Eccentricity: | 0.0064795 |
inclination: | 98.9403° |
perigee height: | 735 km |
apogee height: | 828 km |
right ascension of ascending node: | 17.7932° |
argument of perigee: | 188.3336° |
revolutions per day: | 14.32960510 |
mean anomaly at epoch: | 171.6776° |
orbit number at epoch: | 34679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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