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 29228U 06021A 22178.79805045 .00000822 00000-0 67787-4 0 9991
2 29228 69.9355 102.6535 0002976 2.8057 357.3120 15.03264727883962
Epoch (UTC): | 27 June 2022 19:09:11 |
Eccentricity: | 0.0002976 |
inclination: | 69.9355° |
perigee height: | 555 km |
apogee height: | 559 km |
right ascension of ascending node: | 102.6535° |
argument of perigee: | 2.8057° |
revolutions per day: | 15.03264727 |
mean anomaly at epoch: | 357.3120° |
orbit number at epoch: | 88396 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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