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 59494U 26145.36596473 +.00000000 +00000-0 -75061-5 0 00000
2 59494 43.0015 274.3839 0001507 270.9812 89.0867 15.27588134 06
| Epoch (UTC): | 25 May 2026 08:46:59 |
| Eccentricity: | 0.0001507 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 274.3839° |
| argument of perigee: | 270.9812° |
| revolutions per day: | 15.27588134 |
| mean anomaly at epoch: | 89.0867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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