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 47161U 26145.66668980 +.00000000 +00000-0 +90440-3 0 00009
2 47161 53.0433 249.8329 0007129 310.7079 355.4842 15.82223793 05
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0007129 |
| inclination: | 53.0433° |
| perigee height: | 319 km |
| apogee height: | 329 km |
| right ascension of ascending node: | 249.8329° |
| argument of perigee: | 310.7079° |
| revolutions per day: | 15.82223793 |
| mean anomaly at epoch: | 355.4842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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