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 30119U 99025RY 22176.55660017 .00001008 00000-0 51605-3 0 9996
2 30119 97.9808 288.6823 0150561 36.8462 25.3278 14.11657075792586
Epoch (UTC): | 25 June 2022 13:21:30 |
Eccentricity: | 0.0150561 |
inclination: | 97.9808° |
perigee height: | 745 km |
apogee height: | 962 km |
right ascension of ascending node: | 288.6823° |
argument of perigee: | 36.8462° |
revolutions per day: | 14.11657075 |
mean anomaly at epoch: | 25.3278° |
orbit number at epoch: | 79258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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