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 28898U 05043G 24357.89665775 .00001755 00000-0 35012-3 0 9993
2 28898 98.2769 126.4798 0017864 231.4765 128.4836 14.63152890644060
| Epoch (UTC): | 22 December 2024 21:31:11 |
| Eccentricity: | 0.0017864 |
| inclination: | 98.2769° |
| perigee height: | 670 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 126.4798° |
| argument of perigee: | 231.4765° |
| revolutions per day: | 14.63152890 |
| mean anomaly at epoch: | 128.4836° |
| orbit number at epoch: | 64406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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