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 40567U 95015EA 22222.22879101 .00017075 00000-0 31979-2 0 9993
2 40567 98.7630 3.4974 0065148 93.8306 267.0346 14.63502190388656
| Epoch (UTC): | 10 August 2022 05:29:27 |
| Eccentricity: | 0.0065148 |
| inclination: | 98.7630° |
| perigee height: | 636 km |
| apogee height: | 728 km |
| right ascension of ascending node: | 3.4974° |
| argument of perigee: | 93.8306° |
| revolutions per day: | 14.63502190 |
| mean anomaly at epoch: | 267.0346° |
| orbit number at epoch: | 38865 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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