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 40014U 14033E 22179.56694352 .00002292 00000-0 20420-3 0 9997
2 40014 98.1418 178.4268 0031171 4.0235 356.1216 14.96761241437802
| Epoch (UTC): | 28 June 2022 13:36:23 |
| Eccentricity: | 0.0031171 |
| inclination: | 98.1418° |
| perigee height: | 555 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 178.4268° |
| argument of perigee: | 4.0235° |
| revolutions per day: | 14.96761241 |
| mean anomaly at epoch: | 356.1216° |
| orbit number at epoch: | 43780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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