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 55158U 26145.40686672 +.00000000 +00000-0 -15148-4 0 00008
2 55158 87.8916 25.6002 0002046 92.4242 267.7120 13.11417627 03
| Epoch (UTC): | 25 May 2026 09:45:53 |
| Eccentricity: | 0.0002046 |
| inclination: | 87.8916° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6002° |
| argument of perigee: | 92.4242° |
| revolutions per day: | 13.11417627 |
| mean anomaly at epoch: | 267.7120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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