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 35933U 09051C 22176.84753944 .00000393 00000-0 98546-4 0 9991
2 35933 98.5622 34.6436 0006626 43.4515 316.7204 14.56890247677475
Epoch (UTC): | 25 June 2022 20:20:27 |
Eccentricity: | 0.0006626 |
inclination: | 98.5622° |
perigee height: | 698 km |
apogee height: | 708 km |
right ascension of ascending node: | 34.6436° |
argument of perigee: | 43.4515° |
revolutions per day: | 14.56890247 |
mean anomaly at epoch: | 316.7204° |
orbit number at epoch: | 67747 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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