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 22397U 92093CN 25321.69064125 .00002472 00000-0 95504-3 0 9993
2 22397 70.8021 218.2928 0033963 163.2239 197.0023 14.30852430699551
| Epoch (UTC): | 17 November 2025 16:34:31 |
| Eccentricity: | 0.0033963 |
| inclination: | 70.8021° |
| perigee height: | 764 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 218.2928° |
| argument of perigee: | 163.2239° |
| revolutions per day: | 14.30852430 |
| mean anomaly at epoch: | 197.0023° |
| orbit number at epoch: | 69955 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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