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 59195U 26145.35151003 +.00000000 +00000-0 +14629-4 0 00004
2 59195 43.0024 19.7841 0001243 274.6519 85.4191 15.27584705 00
| Epoch (UTC): | 25 May 2026 08:26:10 |
| Eccentricity: | 0.0001243 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.7841° |
| argument of perigee: | 274.6519° |
| revolutions per day: | 15.27584705 |
| mean anomaly at epoch: | 85.4191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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