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 57618U 26145.02329709 +.00000000 +00000-0 +26630-4 0 00001
2 57618 43.0047 10.2323 0001454 249.5547 110.5148 15.27578409 06
| Epoch (UTC): | 25 May 2026 00:33:32 |
| Eccentricity: | 0.0001454 |
| inclination: | 43.0047° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 10.2323° |
| argument of perigee: | 249.5547° |
| revolutions per day: | 15.27578409 |
| mean anomaly at epoch: | 110.5148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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