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 59531U 26145.56054478 +.00000000 +00000-0 +33759-3 0 00003
2 59531 42.9963 243.7514 0000964 272.2631 87.8110 15.27591471 03
| Epoch (UTC): | 25 May 2026 13:27:11 |
| Eccentricity: | 0.0000964 |
| inclination: | 42.9963° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 243.7514° |
| argument of perigee: | 272.2631° |
| revolutions per day: | 15.27591471 |
| mean anomaly at epoch: | 87.8110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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