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 22220U 26019.22588427 +.00000000 +00000-0 -61665-5 0 00007
2 22220 71.0010 292.5690 0012713 181.5174 340.9769 14.16850395 03
| Epoch (UTC): | 19 January 2026 05:25:16 |
| Eccentricity: | 0.0012713 |
| inclination: | 71.0010° |
| perigee height: | 827 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 292.5690° |
| argument of perigee: | 181.5174° |
| revolutions per day: | 14.16850395 |
| mean anomaly at epoch: | 340.9769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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