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 41187U 26145.41254948 +.00000000 +00000-0 +15525-3 0 00000
2 41187 47.0052 289.8722 0001903 105.8917 254.2179 14.58833572 09
| Epoch (UTC): | 25 May 2026 09:54:04 |
| Eccentricity: | 0.0001903 |
| inclination: | 47.0052° |
| perigee height: | 696 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 289.8722° |
| argument of perigee: | 105.8917° |
| revolutions per day: | 14.58833572 |
| mean anomaly at epoch: | 254.2179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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