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 28480U 04046B 24287.42193705 .00000852 00000-0 33442-3 0 9994
2 28480 98.1722 223.7762 0139143 229.3841 129.5170 14.26567960 35450
Epoch (UTC): | 13 October 2024 10:07:35 |
Eccentricity: | 0.0139143 |
inclination: | 98.1722° |
perigee height: | 703 km |
apogee height: | 903 km |
right ascension of ascending node: | 223.7762° |
argument of perigee: | 229.3841° |
revolutions per day: | 14.26567960 |
mean anomaly at epoch: | 129.5170° |
orbit number at epoch: | 3545 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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