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 68595U 26145.40852253 +.00000000 +00000-0 +78749-3 0 00001
2 68595 51.8698 287.2427 0009519 301.7145 58.2914 15.37547974 00
| Epoch (UTC): | 25 May 2026 09:48:16 |
| Eccentricity: | 0.0009519 |
| inclination: | 51.8698° |
| perigee height: | 447 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 287.2427° |
| argument of perigee: | 301.7145° |
| revolutions per day: | 15.37547974 |
| mean anomaly at epoch: | 58.2914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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