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 39770U 14029E 22177.03966234 .00005917 00000-0 60370-3 0 9995
2 39770 97.9436 294.0302 0009908 64.1472 296.0754 14.90994274438946
| Epoch (UTC): | 26 June 2022 00:57:06 |
| Eccentricity: | 0.0009908 |
| inclination: | 97.9436° |
| perigee height: | 588 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 294.0302° |
| argument of perigee: | 64.1472° |
| revolutions per day: | 14.90994274 |
| mean anomaly at epoch: | 296.0754° |
| orbit number at epoch: | 43894 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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