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 23159.34534140 .00000070 00000-0 34265-4 0 9991
2 11608 81.2140 253.2037 0054886 151.0352 209.3883 14.06266720236518
Epoch (UTC): | 08 June 2023 08:17:17 |
Eccentricity: | 0.0054886 |
inclination: | 81.2140° |
perigee height: | 832 km |
apogee height: | 912 km |
right ascension of ascending node: | 253.2037° |
argument of perigee: | 151.0352° |
revolutions per day: | 14.06266720 |
mean anomaly at epoch: | 209.3883° |
orbit number at epoch: | 23651 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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