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 58088U 26145.61220572 +.00000000 +00000-0 +38248-3 0 00003
2 58088 43.0020 3.1654 0001659 278.1921 81.8742 15.27601542 03
| Epoch (UTC): | 25 May 2026 14:41:34 |
| Eccentricity: | 0.0001659 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.1654° |
| argument of perigee: | 278.1921° |
| revolutions per day: | 15.27601542 |
| mean anomaly at epoch: | 81.8742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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