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 22176.55859983 .00002848 00000-0 25235-3 0 9992
2 40014 98.1414 175.2938 0031382 13.9365 346.2708 14.96749283437352
Epoch (UTC): | 25 June 2022 13:24:23 |
Eccentricity: | 0.0031382 |
inclination: | 98.1414° |
perigee height: | 555 km |
apogee height: | 599 km |
right ascension of ascending node: | 175.2938° |
argument of perigee: | 13.9365° |
revolutions per day: | 14.96749283 |
mean anomaly at epoch: | 346.2708° |
orbit number at epoch: | 43735 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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