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 51147U 26145.45987645 +.00000000 +00000-0 +97870-3 0 00001
2 51147 53.1890 301.8161 0002113 168.8925 191.2123 15.30041267 00
| Epoch (UTC): | 25 May 2026 11:02:13 |
| Eccentricity: | 0.0002113 |
| inclination: | 53.1890° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 301.8161° |
| argument of perigee: | 168.8925° |
| revolutions per day: | 15.30041267 |
| mean anomaly at epoch: | 191.2123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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