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 28931U 06002A 21059.66163186 .00000199 00000-0 47602-4 0 9997
2 28931 97.8746 39.2391 0002023 43.9685 316.1674 14.62803182805157
Epoch (UTC): | 28 February 2021 15:52:44 |
Eccentricity: | 0.0002023 |
inclination: | 97.8746° |
perigee height: | 683 km |
apogee height: | 685 km |
right ascension of ascending node: | 39.2391° |
argument of perigee: | 43.9685° |
revolutions per day: | 14.62803182 |
mean anomaly at epoch: | 316.1674° |
orbit number at epoch: | 80515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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