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 56918U 26145.27723633 +.00000000 +00000-0 +15287-4 0 00000
2 56918 43.0031 357.9408 0001147 257.0463 103.0260 15.27577880 00
| Epoch (UTC): | 25 May 2026 06:39:13 |
| Eccentricity: | 0.0001147 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 357.9408° |
| argument of perigee: | 257.0463° |
| revolutions per day: | 15.27577880 |
| mean anomaly at epoch: | 103.0260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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