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 59146U 26145.37239440 +.00000000 +00000-0 +47116-3 0 00000
2 59146 97.5358 295.6974 0003809 249.2537 110.8311 15.58602800 08
| Epoch (UTC): | 25 May 2026 08:56:14 |
| Eccentricity: | 0.0003809 |
| inclination: | 97.5358° |
| perigee height: | 389 km |
| apogee height: | 394 km |
| right ascension of ascending node: | 295.6974° |
| argument of perigee: | 249.2537° |
| revolutions per day: | 15.58602800 |
| mean anomaly at epoch: | 110.8311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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