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 58808U 26145.53850661 +.00000000 +00000-0 +65610-5 0 00007
2 58808 43.0007 90.8432 0000791 261.7891 98.2871 15.27575104 04
| Epoch (UTC): | 25 May 2026 12:55:26 |
| Eccentricity: | 0.0000791 |
| inclination: | 43.0007° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 90.8432° |
| argument of perigee: | 261.7891° |
| revolutions per day: | 15.27575104 |
| mean anomaly at epoch: | 98.2871° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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