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 30171U 99025UC 24279.66210798 .00001952 00000-0 12464-2 0 9996
2 30171 98.4544 167.1391 0187331 38.2449 323.1834 13.96308887902254
Epoch (UTC): | 05 October 2024 15:53:26 |
Eccentricity: | 0.0187331 |
inclination: | 98.4544° |
perigee height: | 770 km |
apogee height: | 1043 km |
right ascension of ascending node: | 167.1391° |
argument of perigee: | 38.2449° |
revolutions per day: | 13.96308887 |
mean anomaly at epoch: | 323.1834° |
orbit number at epoch: | 90225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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