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 22219U 26049.42165025 +.00000000 +00000-0 +15015-3 0 00000
2 22219 71.0585 58.3484 0019903 232.9567 126.9735 14.14079168 06
| Epoch (UTC): | 18 February 2026 10:07:10 |
| Eccentricity: | 0.0019903 |
| inclination: | 71.0585° |
| perigee height: | 831 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 58.3484° |
| argument of perigee: | 232.9567° |
| revolutions per day: | 14.14079168 |
| mean anomaly at epoch: | 126.9735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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