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 26039.51822140 +.00000000 +00000-0 -32289-4 0 00001
2 22219 71.0583 79.0541 0020335 247.1455 112.7520 14.14076528 05
| Epoch (UTC): | 08 February 2026 12:26:14 |
| Eccentricity: | 0.0020335 |
| inclination: | 71.0583° |
| perigee height: | 831 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 79.0541° |
| argument of perigee: | 247.1455° |
| revolutions per day: | 14.14076528 |
| mean anomaly at epoch: | 112.7520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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