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 29658U 06060A 21089.80007632 0.00001300 00000-0 48248-4 0 05
2 29658 98.1539 288.5942 0000519 3.7086 356.2912 15.27615302 04
Epoch (UTC): | 30 March 2021 19:12:06 |
Eccentricity: | 0.0000519 |
inclination: | 98.1539° |
perigee height: | 482 km |
apogee height: | 483 km |
right ascension of ascending node: | 288.5942° |
argument of perigee: | 3.7086° |
revolutions per day: | 15.27615302 |
mean anomaly at epoch: | 356.2912° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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