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 63568U 26145.42411031 +.00000000 +00000-0 +91639-3 0 00006
2 63568 42.9936 197.1867 0001312 111.2571 248.8421 15.27571329 08
| Epoch (UTC): | 25 May 2026 10:10:43 |
| Eccentricity: | 0.0001312 |
| inclination: | 42.9936° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.1867° |
| argument of perigee: | 111.2571° |
| revolutions per day: | 15.27571329 |
| mean anomaly at epoch: | 248.8421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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