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 22177.48408263 .00000147 00000-0 10356-3 0 9993
2 28654 98.9488 247.9129 0013260 308.5991 51.3993 14.12746179881250
| Epoch (UTC): | 26 June 2022 11:37:04 |
| Eccentricity: | 0.0013260 |
| inclination: | 98.9488° |
| perigee height: | 840 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 247.9129° |
| argument of perigee: | 308.5991° |
| revolutions per day: | 14.12746179 |
| mean anomaly at epoch: | 51.3993° |
| orbit number at epoch: | 88125 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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