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 59367U 26145.44472586 +.00000000 +00000-0 +45308-4 0 00005
2 59367 43.0026 186.2015 0001601 262.2254 97.8416 15.27573154 06
| Epoch (UTC): | 25 May 2026 10:40:24 |
| Eccentricity: | 0.0001601 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.2015° |
| argument of perigee: | 262.2254° |
| revolutions per day: | 15.27573154 |
| mean anomaly at epoch: | 97.8416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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