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 51U 60009C 23271.97286823 -.00000012 00000-0 71000-3 0 9996
2 51 47.2110 239.4512 0105636 126.2775 234.7826 12.18303480810191
Epoch (UTC): | 28 September 2023 23:20:55 |
Eccentricity: | 0.0105636 |
inclination: | 47.2110° |
perigee height: | 1515 km |
apogee height: | 1684 km |
right ascension of ascending node: | 239.4512° |
argument of perigee: | 126.2775° |
revolutions per day: | 12.18303480 |
mean anomaly at epoch: | 234.7826° |
orbit number at epoch: | 81019 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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