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 28654U 05018A 23332.13437329 .00000401 00000-0 23836-3 0 9994
2 28654 98.8962 45.6230 0013287 275.8607 84.1050 14.13065000954720
| Epoch (UTC): | 28 November 2023 03:13:29 |
| Eccentricity: | 0.0013287 |
| inclination: | 98.8962° |
| perigee height: | 839 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 45.6230° |
| argument of perigee: | 275.8607° |
| revolutions per day: | 14.13065000 |
| mean anomaly at epoch: | 84.1050° |
| orbit number at epoch: | 95472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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