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 22179.65697110 .00004658 00000-0 47638-3 0 9992
2 39770 97.9437 296.6644 0009429 58.6741 301.5386 14.91010540439332
| Epoch (UTC): | 28 June 2022 15:46:02 |
| Eccentricity: | 0.0009429 |
| inclination: | 97.9437° |
| perigee height: | 588 km |
| apogee height: | 601 km |
| right ascension of ascending node: | 296.6644° |
| argument of perigee: | 58.6741° |
| revolutions per day: | 14.91010540 |
| mean anomaly at epoch: | 301.5386° |
| orbit number at epoch: | 43933 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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