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 58194U 26145.48353554 +.00000000 +00000-0 +10822-4 0 00002
2 58194 43.0021 69.3481 0001146 272.3905 87.6815 15.27574417 08
| Epoch (UTC): | 25 May 2026 11:36:17 |
| Eccentricity: | 0.0001146 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.3481° |
| argument of perigee: | 272.3905° |
| revolutions per day: | 15.27574417 |
| mean anomaly at epoch: | 87.6815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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