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 21017.18316313 .00000134 00000-0 34858-4 0 9998
2 28931 97.8675 358.7103 0001868 93.6636 266.4767 14.62787208798940
Epoch (UTC): | 17 January 2021 04:23:45 |
Eccentricity: | 0.0001868 |
inclination: | 97.8675° |
perigee height: | 683 km |
apogee height: | 685 km |
right ascension of ascending node: | 358.7103° |
argument of perigee: | 93.6636° |
revolutions per day: | 14.62787208 |
mean anomaly at epoch: | 266.4767° |
orbit number at epoch: | 79894 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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