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 11608U 79095B 24278.71223501 .00000322 00000-0 18525-3 0 9991
2 11608 81.2127 143.0023 0053180 230.5487 129.0971 14.06409123304598
Epoch (UTC): | 04 October 2024 17:05:37 |
Eccentricity: | 0.0053180 |
inclination: | 81.2127° |
perigee height: | 833 km |
apogee height: | 910 km |
right ascension of ascending node: | 143.0023° |
argument of perigee: | 230.5487° |
revolutions per day: | 14.06409123 |
mean anomaly at epoch: | 129.0971° |
orbit number at epoch: | 30459 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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