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 22369U 92093BJ 24357.85120355 .00000051 00000-0 69690-4 0 9995
2 22369 70.8846 152.0721 0098816 45.3602 315.5511 13.94380256626610
Epoch (UTC): | 22 December 2024 20:25:43 |
Eccentricity: | 0.0098816 |
inclination: | 70.8846° |
perigee height: | 841 km |
apogee height: | 985 km |
right ascension of ascending node: | 152.0721° |
argument of perigee: | 45.3602° |
revolutions per day: | 13.94380256 |
mean anomaly at epoch: | 315.5511° |
orbit number at epoch: | 62661 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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