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 22081U 26106.28013875 +.00000000 +00000-0 +70197-4 0 00003
2 22081 74.0421 300.9558 0035754 201.0798 158.8883 14.34844013 07
| Epoch (UTC): | 16 April 2026 06:43:23 |
| Eccentricity: | 0.0035754 |
| inclination: | 74.0421° |
| perigee height: | 750 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 300.9558° |
| argument of perigee: | 201.0798° |
| revolutions per day: | 14.34844013 |
| mean anomaly at epoch: | 158.8883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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