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 57918U 26145.26887752 +.00000000 +00000-0 -12254-5 0 00006
2 57918 43.0025 107.7426 0001366 271.5809 88.4886 15.27575501 01
| Epoch (UTC): | 25 May 2026 06:27:11 |
| Eccentricity: | 0.0001366 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.7426° |
| argument of perigee: | 271.5809° |
| revolutions per day: | 15.27575501 |
| mean anomaly at epoch: | 88.4886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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