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 27432U 02024C 21018.86208237 -.00000033 00000-0 71506-5 0 9995
2 27432 99.0899 30.7288 0049550 289.1389 142.5363 14.14102940964093
Epoch (UTC): | 18 January 2021 20:41:23 |
Eccentricity: | 0.0049550 |
inclination: | 99.0899° |
perigee height: | 809 km |
apogee height: | 881 km |
right ascension of ascending node: | 30.7288° |
argument of perigee: | 289.1389° |
revolutions per day: | 14.14102940 |
mean anomaly at epoch: | 142.5363° |
orbit number at epoch: | 96409 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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