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 29507U 06046C 21019.07197269 .00000262 00000-0 25205-4 0 9991
2 29507 97.7173 45.8777 0046411 156.7051 203.6290 15.00621305777756
Epoch (UTC): | 19 January 2021 01:43:38 |
Eccentricity: | 0.0046411 |
inclination: | 97.7173° |
perigee height: | 533 km |
apogee height: | 597 km |
right ascension of ascending node: | 45.8777° |
argument of perigee: | 156.7051° |
revolutions per day: | 15.00621305 |
mean anomaly at epoch: | 203.6290° |
orbit number at epoch: | 77775 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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