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 57637U 26145.01423198 +.00000000 +00000-0 +79253-4 0 00007
2 57637 43.0027 21.1348 0001314 273.2845 86.7856 15.27576433 08
| Epoch (UTC): | 25 May 2026 00:20:29 |
| Eccentricity: | 0.0001314 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 21.1348° |
| argument of perigee: | 273.2845° |
| revolutions per day: | 15.27576433 |
| mean anomaly at epoch: | 86.7856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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