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 58868U 26145.55257911 +.00000000 +00000-0 +17276-3 0 00007
2 58868 43.0005 175.1796 0001300 269.7876 90.2826 15.27572772 06
| Epoch (UTC): | 25 May 2026 13:15:42 |
| Eccentricity: | 0.0001300 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.1796° |
| argument of perigee: | 269.7876° |
| revolutions per day: | 15.27572772 |
| mean anomaly at epoch: | 90.2826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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