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 59645U 26145.60662200 +.00000000 +00000-0 -27474-3 0 00000
2 59645 43.0064 6.8563 0001090 286.1358 73.9374 15.27613727 03
| Epoch (UTC): | 25 May 2026 14:33:32 |
| Eccentricity: | 0.0001090 |
| inclination: | 43.0064° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 6.8563° |
| argument of perigee: | 286.1358° |
| revolutions per day: | 15.27613727 |
| mean anomaly at epoch: | 73.9374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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