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 22176.10183761 .00000731 00000-0 99785-4 0 9995
2 40071 98.4084 45.2208 0007258 297.8400 62.2074 14.81881257430474
| Epoch (UTC): | 25 June 2022 02:26:38 |
| Eccentricity: | 0.0007258 |
| inclination: | 98.4084° |
| perigee height: | 618 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 45.2208° |
| argument of perigee: | 297.8400° |
| revolutions per day: | 14.81881257 |
| mean anomaly at epoch: | 62.2074° |
| orbit number at epoch: | 43047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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