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 28222U 26158.71209345 +.00000000 +00000-0 +57470-3 0 00008
2 28222 97.7086 233.2873 0008767 326.5186 33.5524 15.77195190 09
| Epoch (UTC): | 07 June 2026 17:05:24 |
| Eccentricity: | 0.0008767 |
| inclination: | 97.7086° |
| perigee height: | 333 km |
| apogee height: | 344 km |
| right ascension of ascending node: | 233.2873° |
| argument of perigee: | 326.5186° |
| revolutions per day: | 15.77195190 |
| mean anomaly at epoch: | 33.5524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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