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 23081.79746183 .00025277 00000-0 21337-2 0 9992
2 39770 97.9563 206.8661 0009507 240.3744 119.6395 14.98071383479201
| Epoch (UTC): | 22 March 2023 19:08:20 |
| Eccentricity: | 0.0009507 |
| inclination: | 97.9563° |
| perigee height: | 566 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 206.8661° |
| argument of perigee: | 240.3744° |
| revolutions per day: | 14.98071383 |
| mean anomaly at epoch: | 119.6395° |
| orbit number at epoch: | 47920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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