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 22180.59650891 .00004295 00000-0 43973-3 0 9997
2 39770 97.9441 297.6101 0009565 55.3527 304.8531 14.91016073439473
| Epoch (UTC): | 29 June 2022 14:18:58 |
| Eccentricity: | 0.0009565 |
| inclination: | 97.9441° |
| perigee height: | 588 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 297.6101° |
| argument of perigee: | 55.3527° |
| revolutions per day: | 14.91016073 |
| mean anomaly at epoch: | 304.8531° |
| orbit number at epoch: | 43947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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