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 57937U 26145.66668980 +.00000000 +00000-0 +18349-2 0 00008
2 57937 53.1594 26.6221 0001174 83.4507 108.9214 15.33490370 09
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001174 |
| inclination: | 53.1594° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 26.6221° |
| argument of perigee: | 83.4507° |
| revolutions per day: | 15.33490370 |
| mean anomaly at epoch: | 108.9214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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