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 58668U 26145.35875330 +.00000000 +00000-0 +25128-4 0 00000
2 58668 43.0038 11.9946 0001194 262.5541 97.5175 15.27578780 07
| Epoch (UTC): | 25 May 2026 08:36:36 |
| Eccentricity: | 0.0001194 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 11.9946° |
| argument of perigee: | 262.5541° |
| revolutions per day: | 15.27578780 |
| mean anomaly at epoch: | 97.5175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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