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 61905U 26145.59645082 +.00000000 +00000-0 +25993-3 0 00002
2 61905 97.3847 220.2474 0006533 46.8891 313.2895 15.29100175 07
| Epoch (UTC): | 25 May 2026 14:18:53 |
| Eccentricity: | 0.0006533 |
| inclination: | 97.3847° |
| perigee height: | 474 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 220.2474° |
| argument of perigee: | 46.8891° |
| revolutions per day: | 15.29100175 |
| mean anomaly at epoch: | 313.2895° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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