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 59587U 26145.56895036 +.00000000 +00000-0 +39493-3 0 00008
2 59587 97.3489 229.5516 0010137 115.1614 245.0683 15.37794747 09
| Epoch (UTC): | 25 May 2026 13:39:17 |
| Eccentricity: | 0.0010137 |
| inclination: | 97.3489° |
| perigee height: | 446 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 229.5516° |
| argument of perigee: | 115.1614° |
| revolutions per day: | 15.37794747 |
| mean anomaly at epoch: | 245.0683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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