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 59414U 26145.51212928 +.00000000 +00000-0 +25837-4 0 00003
2 59414 43.0031 335.4682 0001044 265.1809 94.8924 15.27574022 08
| Epoch (UTC): | 25 May 2026 12:17:27 |
| Eccentricity: | 0.0001044 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 335.4682° |
| argument of perigee: | 265.1809° |
| revolutions per day: | 15.27574022 |
| mean anomaly at epoch: | 94.8924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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