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 25338U 98030A 24310.69403134 .00000749 00000-0 32669-3 0 9990
2 25338 98.5576 334.8110 0009146 271.1995 88.8138 14.26782205377614
Epoch (UTC): | 05 November 2024 16:39:24 |
Eccentricity: | 0.0009146 |
inclination: | 98.5576° |
perigee height: | 796 km |
apogee height: | 809 km |
right ascension of ascending node: | 334.8110° |
argument of perigee: | 271.1995° |
revolutions per day: | 14.26782205 |
mean anomaly at epoch: | 88.8138° |
orbit number at epoch: | 37761 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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