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 57993U 26145.30206155 +.00000000 +00000-0 +40665-4 0 00001
2 57993 43.0068 354.3608 0001860 275.5571 84.5069 15.27591417 06
| Epoch (UTC): | 25 May 2026 07:14:58 |
| Eccentricity: | 0.0001860 |
| inclination: | 43.0068° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 354.3608° |
| argument of perigee: | 275.5571° |
| revolutions per day: | 15.27591417 |
| mean anomaly at epoch: | 84.5069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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