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 28353U 04021B 24348.86260815 .00000152 00000-0 10407-3 0 9998
2 28353 71.0001 98.5201 0005307 340.3001 19.7915 14.14491466 59087
| Epoch (UTC): | 13 December 2024 20:42:09 |
| Eccentricity: | 0.0005307 |
| inclination: | 71.0001° |
| perigee height: | 840 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 98.5201° |
| argument of perigee: | 340.3001° |
| revolutions per day: | 14.14491466 |
| mean anomaly at epoch: | 19.7915° |
| orbit number at epoch: | 5908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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