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 26042.06481860 +.00000000 +00000-0 +13765-4 0 00002
2 22219 71.0580 73.7299 0020220 243.4460 116.4590 14.14076532 04
| Epoch (UTC): | 11 February 2026 01:33:20 |
| Eccentricity: | 0.0020220 |
| inclination: | 71.0580° |
| perigee height: | 831 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 73.7299° |
| argument of perigee: | 243.4460° |
| revolutions per day: | 14.14076532 |
| mean anomaly at epoch: | 116.4590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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