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 26129.78009463 +.00000000 +00000-0 +26851-4 0 00002
2 22219 71.0616 250.3585 0015897 108.7098 251.5751 14.14103490 03
| Epoch (UTC): | 09 May 2026 18:43:20 |
| Eccentricity: | 0.0015897 |
| inclination: | 71.0616° |
| perigee height: | 834 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 250.3585° |
| argument of perigee: | 108.7098° |
| revolutions per day: | 14.14103490 |
| mean anomaly at epoch: | 251.5751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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