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 26044.46993789 +.00000000 +00000-0 +73495-4 0 00002
2 22219 71.0578 68.7008 0020136 239.9094 120.0032 14.14077040 09
| Epoch (UTC): | 13 February 2026 11:16:42 |
| Eccentricity: | 0.0020136 |
| inclination: | 71.0578° |
| perigee height: | 831 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 68.7008° |
| argument of perigee: | 239.9094° |
| revolutions per day: | 14.14077040 |
| mean anomaly at epoch: | 120.0032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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