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 28654U 05018A 24256.78430021 .00001237 00000-0 68245-3 0 9994
2 28654 98.8690 333.0054 0014510 171.2693 188.8734 14.13327438995632
Epoch (UTC): | 12 September 2024 18:49:23 |
Eccentricity: | 0.0014510 |
inclination: | 98.8690° |
perigee height: | 837 km |
apogee height: | 858 km |
right ascension of ascending node: | 333.0054° |
argument of perigee: | 171.2693° |
revolutions per day: | 14.13327438 |
mean anomaly at epoch: | 188.8734° |
orbit number at epoch: | 99563 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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