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 is defined by the following mean orbital elements,
1 42201U 81053TR 24246.55754680 .00041033 00000-0 15931-1 0 9995
2 42201 82.7009 350.4008 0039221 139.7857 220.6243 14.29227364557594
| Epoch (UTC): | 02 September 2024 13:22:52 |
| Eccentricity: | 0.0039221 |
| inclination: | 82.7009° |
| perigee height: | 766 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 350.4008° |
| argument of perigee: | 139.7857° |
| revolutions per day: | 14.29227364 |
| mean anomaly at epoch: | 220.6243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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