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 45157U 26145.44603447 +.00000000 +00000-0 -14097-3 0 00000
2 45157 87.8855 40.8120 0002341 80.9428 279.1965 13.10377663 07
| Epoch (UTC): | 25 May 2026 10:42:17 |
| Eccentricity: | 0.0002341 |
| inclination: | 87.8855° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8120° |
| argument of perigee: | 80.9428° |
| revolutions per day: | 13.10377663 |
| mean anomaly at epoch: | 279.1965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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