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 22430U 92093DX 24280.41245424 .00001440 00000-0 10296-2 0 9995
2 22430 71.2387 29.5253 0117283 258.5530 168.5813 13.95592601614124
Epoch (UTC): | 06 October 2024 09:53:56 |
Eccentricity: | 0.0117283 |
inclination: | 71.2387° |
perigee height: | 823 km |
apogee height: | 994 km |
right ascension of ascending node: | 29.5253° |
argument of perigee: | 258.5530° |
revolutions per day: | 13.95592601 |
mean anomaly at epoch: | 168.5813° |
orbit number at epoch: | 61412 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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