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 870U 64051A 22224.13356933 .00000048 00000-0 30926-4 0 9992
2 870 79.8999 7.1013 0097448 15.2129 345.1919 13.91235098938500
| Epoch (UTC): | 12 August 2022 03:12:20 |
| Eccentricity: | 0.0097448 |
| inclination: | 79.8999° |
| perigee height: | 853 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 7.1013° |
| argument of perigee: | 15.2129° |
| revolutions per day: | 13.91235098 |
| mean anomaly at epoch: | 345.1919° |
| orbit number at epoch: | 93850 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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