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 58944U 26145.49377674 +.00000000 +00000-0 +42125-4 0 00006
2 58944 53.1610 313.1371 0001015 82.2334 277.8782 15.30198917 01
| Epoch (UTC): | 25 May 2026 11:51:02 |
| Eccentricity: | 0.0001015 |
| inclination: | 53.1610° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.1371° |
| argument of perigee: | 82.2334° |
| revolutions per day: | 15.30198917 |
| mean anomaly at epoch: | 277.8782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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