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 56697U 26145.45877897 +.00000000 +00000-0 +13341-3 0 00004
2 56697 43.0019 197.2688 0000487 333.8961 26.1867 15.27589842 06
| Epoch (UTC): | 25 May 2026 11:00:38 |
| Eccentricity: | 0.0000487 |
| inclination: | 43.0019° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 197.2688° |
| argument of perigee: | 333.8961° |
| revolutions per day: | 15.27589842 |
| mean anomaly at epoch: | 26.1867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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