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 24297U 96051A 24282.88729284 .00000183 00000-0 12196-3 0 9995
2 24297 70.9040 192.7343 0023250 164.3589 195.8256 14.13636438449195
Epoch (UTC): | 08 October 2024 21:17:42 |
Eccentricity: | 0.0023250 |
inclination: | 70.9040° |
perigee height: | 830 km |
apogee height: | 864 km |
right ascension of ascending node: | 192.7343° |
argument of perigee: | 164.3589° |
revolutions per day: | 14.13636438 |
mean anomaly at epoch: | 195.8256° |
orbit number at epoch: | 44919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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