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 59194U 26145.37321025 +.00000000 +00000-0 +85047-4 0 00000
2 59194 43.0045 19.0864 0002096 268.9011 91.1601 15.27579444 04
| Epoch (UTC): | 25 May 2026 08:57:25 |
| Eccentricity: | 0.0002096 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.0864° |
| argument of perigee: | 268.9011° |
| revolutions per day: | 15.27579444 |
| mean anomaly at epoch: | 91.1601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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