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 55620U 26145.41368627 +.00000000 +00000-0 +58518-4 0 00007
2 55620 43.0005 280.8948 0001413 259.4449 100.6244 15.27581823 06
| Epoch (UTC): | 25 May 2026 09:55:42 |
| Eccentricity: | 0.0001413 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.8948° |
| argument of perigee: | 259.4449° |
| revolutions per day: | 15.27581823 |
| mean anomaly at epoch: | 100.6244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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