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 58493U 26145.54997704 +.00000000 +00000-0 +21951-3 0 00006
2 58493 43.0048 349.3536 0001602 260.8729 99.1942 15.27586559 03
| Epoch (UTC): | 25 May 2026 13:11:58 |
| Eccentricity: | 0.0001602 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 349.3536° |
| argument of perigee: | 260.8729° |
| revolutions per day: | 15.27586559 |
| mean anomaly at epoch: | 99.1942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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