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 59887U 26145.47011053 +.00000000 +00000-0 +37133-4 0 00000
2 59887 43.0058 55.7168 0001080 278.7269 81.3460 15.27567427 09
| Epoch (UTC): | 25 May 2026 11:16:57 |
| Eccentricity: | 0.0001080 |
| inclination: | 43.0058° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 55.7168° |
| argument of perigee: | 278.7269° |
| revolutions per day: | 15.27567427 |
| mean anomaly at epoch: | 81.3460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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