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 40014U 14033E 22180.97083456 .00001751 00000-0 15734-3 0 9992
2 40014 98.1419 179.8901 0030954 359.4712 0.6469 14.96762949438018
Epoch (UTC): | 29 June 2022 23:18:00 |
Eccentricity: | 0.0030954 |
inclination: | 98.1419° |
perigee height: | 555 km |
apogee height: | 598 km |
right ascension of ascending node: | 179.8901° |
argument of perigee: | 359.4712° |
revolutions per day: | 14.96762949 |
mean anomaly at epoch: | 0.6469° |
orbit number at epoch: | 43801 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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