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 55622U 26145.41755458 +.00000000 +00000-0 -20455-4 0 00001
2 55622 43.0017 280.9263 0001339 284.4320 75.6383 15.27577287 09
| Epoch (UTC): | 25 May 2026 10:01:16 |
| Eccentricity: | 0.0001339 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.9263° |
| argument of perigee: | 284.4320° |
| revolutions per day: | 15.27577287 |
| mean anomaly at epoch: | 75.6383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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