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 42789U 17036AA 21023.42084612 .00001493 00000-0 63799-4 0 9997
2 42789 97.2733 77.6337 0010225 338.0813 21.9986 15.24332071199295
Epoch (UTC): | 23 January 2021 10:06:01 |
Eccentricity: | 0.0010225 |
inclination: | 97.2733° |
perigee height: | 486 km |
apogee height: | 500 km |
right ascension of ascending node: | 77.6337° |
argument of perigee: | 338.0813° |
revolutions per day: | 15.24332071 |
mean anomaly at epoch: | 21.9986° |
orbit number at epoch: | 19929 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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