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 22179.46713765 .00000126 00000-0 91927-4 0 9990
2 28654 98.9488 249.8944 0013215 302.5301 57.4593 14.12746762881537
| Epoch (UTC): | 28 June 2022 11:12:40 |
| Eccentricity: | 0.0013215 |
| inclination: | 98.9488° |
| perigee height: | 840 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 249.8944° |
| argument of perigee: | 302.5301° |
| revolutions per day: | 14.12746762 |
| mean anomaly at epoch: | 57.4593° |
| orbit number at epoch: | 88153 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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