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 22566U 26071.81904072 +.00000000 +00000-0 +10064-4 0 00006
2 22566 71.0079 208.6082 0012038 309.9663 50.0401 14.15309352 06
| Epoch (UTC): | 12 March 2026 19:39:25 |
| Eccentricity: | 0.0012038 |
| inclination: | 71.0079° |
| perigee height: | 833 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 208.6082° |
| argument of perigee: | 309.9663° |
| revolutions per day: | 14.15309352 |
| mean anomaly at epoch: | 50.0401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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