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 43056U 26142.49716081 +.00000000 +00000-0 +00000-0 0 00002
2 43056 55.0811 222.2139 0003659 275.5669 84.4487 1.70474676 01
| Epoch (UTC): | 22 May 2026 11:55:54 |
| Eccentricity: | 0.0003659 |
| inclination: | 55.0811° |
| perigee height: | 23211 km |
| apogee height: | 23233 km |
| right ascension of ascending node: | 222.2139° |
| argument of perigee: | 275.5669° |
| revolutions per day: | 1.70474676 |
| mean anomaly at epoch: | 84.4487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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