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 30274U 99025YK 23090.55317530 .00008950 00000-0 34547-2 0 9991
2 30274 99.3347 124.3818 0005238 170.4761 352.3590 14.30427692840214
Epoch (UTC): | 31 March 2023 13:16:34 |
Eccentricity: | 0.0005238 |
inclination: | 99.3347° |
perigee height: | 786 km |
apogee height: | 794 km |
right ascension of ascending node: | 124.3818° |
argument of perigee: | 170.4761° |
revolutions per day: | 14.30427692 |
mean anomaly at epoch: | 352.3590° |
orbit number at epoch: | 84021 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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