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 28908U 05048A 23088.22511906 .00000039 00000-0 17473-3 0 9998
2 28908 82.4723 339.6255 0006882 280.2356 203.4347 12.55532813791328
| Epoch (UTC): | 29 March 2023 05:24:10 |
| Eccentricity: | 0.0006882 |
| inclination: | 82.4723° |
| perigee height: | 1436 km |
| apogee height: | 1447 km |
| right ascension of ascending node: | 339.6255° |
| argument of perigee: | 280.2356° |
| revolutions per day: | 12.55532813 |
| mean anomaly at epoch: | 203.4347° |
| orbit number at epoch: | 79132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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