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 56906U 26145.01055172 +.00000000 +00000-0 -29666-4 0 00002
2 56906 43.0033 359.3878 0001284 262.3347 97.7359 15.27574126 06
| Epoch (UTC): | 25 May 2026 00:15:11 |
| Eccentricity: | 0.0001284 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 359.3878° |
| argument of perigee: | 262.3347° |
| revolutions per day: | 15.27574126 |
| mean anomaly at epoch: | 97.7359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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