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 24298U 96051B 22225.53743489 .00000074 00000-0 66658-4 0 9998
2 24298 70.8204 50.3485 0019081 261.4612 98.4346 14.12423719337498
Epoch (UTC): | 13 August 2022 12:53:54 |
Eccentricity: | 0.0019081 |
inclination: | 70.8204° |
perigee height: | 837 km |
apogee height: | 865 km |
right ascension of ascending node: | 50.3485° |
argument of perigee: | 261.4612° |
revolutions per day: | 14.12423719 |
mean anomaly at epoch: | 98.4346° |
orbit number at epoch: | 33749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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