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 18422U 87088B 23159.62383009 .00000593 00000-0 68748-4 0 9993
2 18422 82.5110 291.3305 0020899 89.5427 270.8182 14.83588576904200
| Epoch (UTC): | 08 June 2023 14:58:18 |
| Eccentricity: | 0.0020899 |
| inclination: | 82.5110° |
| perigee height: | 603 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 291.3305° |
| argument of perigee: | 89.5427° |
| revolutions per day: | 14.83588576 |
| mean anomaly at epoch: | 270.8182° |
| orbit number at epoch: | 90420 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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