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 22220U 92076B 25197.82904718 .00000130 00000-0 88774-4 0 9997
2 22220 71.0018 325.1915 0010644 95.2580 18.9675 14.16811636688428
| Epoch (UTC): | 16 July 2025 19:53:49 |
| Eccentricity: | 0.0010644 |
| inclination: | 71.0018° |
| perigee height: | 828 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 325.1915° |
| argument of perigee: | 95.2580° |
| revolutions per day: | 14.16811636 |
| mean anomaly at epoch: | 18.9675° |
| orbit number at epoch: | 68842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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