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 40071U 14037C 22179.47795534 .00000596 00000-0 82781-4 0 9992
2 40071 98.4084 48.7647 0007161 285.7397 74.3025 14.81884679430979
| Epoch (UTC): | 28 June 2022 11:28:15 |
| Eccentricity: | 0.0007161 |
| inclination: | 98.4084° |
| perigee height: | 618 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 48.7647° |
| argument of perigee: | 285.7397° |
| revolutions per day: | 14.81884679 |
| mean anomaly at epoch: | 74.3025° |
| orbit number at epoch: | 43097 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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