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 24255.51400851 .00000442 00000-0 25533-3 0 9991
2 28353 70.9995 294.3792 0004369 169.9928 190.1282 14.14447195 45882
| Epoch (UTC): | 11 September 2024 12:20:10 |
| Eccentricity: | 0.0004369 |
| inclination: | 70.9995° |
| perigee height: | 841 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 294.3792° |
| argument of perigee: | 169.9928° |
| revolutions per day: | 14.14447195 |
| mean anomaly at epoch: | 190.1282° |
| orbit number at epoch: | 4588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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