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 59196U 26145.37707043 +.00000000 +00000-0 +52080-4 0 00001
2 59196 43.0062 19.1135 0001253 241.9000 118.1725 15.27571150 03
| Epoch (UTC): | 25 May 2026 09:02:58 |
| Eccentricity: | 0.0001253 |
| inclination: | 43.0062° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.1135° |
| argument of perigee: | 241.9000° |
| revolutions per day: | 15.27571150 |
| mean anomaly at epoch: | 118.1725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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