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 57875U 26145.51211078 +.00000000 +00000-0 +40996-4 0 00000
2 57875 43.0039 211.5910 0002018 283.9965 76.0662 15.27576766 04
| Epoch (UTC): | 25 May 2026 12:17:26 |
| Eccentricity: | 0.0002018 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.5910° |
| argument of perigee: | 283.9965° |
| revolutions per day: | 15.27576766 |
| mean anomaly at epoch: | 76.0662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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