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 22076U 26150.54367558 +.00000000 +00000-0 +13651-3 0 00006
2 22076 66.0384 168.8249 0008362 270.2845 261.2295 12.81093664 08
| Epoch (UTC): | 30 May 2026 13:02:53 |
| Eccentricity: | 0.0008362 |
| inclination: | 66.0384° |
| perigee height: | 1331 km |
| apogee height: | 1344 km |
| right ascension of ascending node: | 168.8249° |
| argument of perigee: | 270.2845° |
| revolutions per day: | 12.81093664 |
| mean anomaly at epoch: | 261.2295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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