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 58494U 26145.61151458 +.00000000 +00000-0 +16643-4 0 00006
2 58494 43.0031 348.9515 0001073 262.3366 97.7364 15.27574202 08
| Epoch (UTC): | 25 May 2026 14:40:34 |
| Eccentricity: | 0.0001073 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 348.9515° |
| argument of perigee: | 262.3366° |
| revolutions per day: | 15.27574202 |
| mean anomaly at epoch: | 97.7364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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