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 33683U 99025DFU 22175.83181020 .00003573 00000-0 99853-3 0 9993
2 33683 98.2627 28.0591 0072991 82.6914 278.2566 14.45218811745223
Epoch (UTC): | 24 June 2022 19:57:48 |
Eccentricity: | 0.0072991 |
inclination: | 98.2627° |
perigee height: | 689 km |
apogee height: | 793 km |
right ascension of ascending node: | 28.0591° |
argument of perigee: | 82.6914° |
revolutions per day: | 14.45218811 |
mean anomaly at epoch: | 278.2566° |
orbit number at epoch: | 74522 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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