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 33272U 08037A 22225.45912815 .00000072 00000-0 28570-4 0 9998
2 33272 98.1518 175.7607 0016091 344.7407 15.3301 14.51954141744261
Epoch (UTC): | 13 August 2022 11:01:08 |
Eccentricity: | 0.0016091 |
inclination: | 98.1518° |
perigee height: | 708 km |
apogee height: | 730 km |
right ascension of ascending node: | 175.7607° |
argument of perigee: | 344.7407° |
revolutions per day: | 14.51954141 |
mean anomaly at epoch: | 15.3301° |
orbit number at epoch: | 74426 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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