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 22177.12996554 .00000156 00000-0 10809-3 0 9992
2 28654 98.9488 247.5591 0013272 309.6678 50.3322 14.12746142881295
| Epoch (UTC): | 26 June 2022 03:07:09 |
| Eccentricity: | 0.0013272 |
| inclination: | 98.9488° |
| perigee height: | 840 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 247.5591° |
| argument of perigee: | 309.6678° |
| revolutions per day: | 14.12746142 |
| mean anomaly at epoch: | 50.3322° |
| orbit number at epoch: | 88129 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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