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 22116U 26152.22283963 +.00000000 +00000-0 +00000-0 0 00006
2 22116 14.1831 10.3839 0005091 332.4029 30.8456 0.99314512 04
| Epoch (UTC): | 01 June 2026 05:20:53 |
| Eccentricity: | 0.0005091 |
| inclination: | 14.1831° |
| perigee height: | 36036 km |
| apogee height: | 36079 km |
| right ascension of ascending node: | 10.3839° |
| argument of perigee: | 332.4029° |
| revolutions per day: | 0.99314512 |
| mean anomaly at epoch: | 30.8456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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