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 61534U 26145.39035973 +.00000000 +00000-0 +15039-4 0 00001
2 61534 53.1605 218.1856 0000776 99.8989 260.2116 15.69709982 08
| Epoch (UTC): | 25 May 2026 09:22:07 |
| Eccentricity: | 0.0000776 |
| inclination: | 53.1605° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 218.1856° |
| argument of perigee: | 99.8989° |
| revolutions per day: | 15.69709982 |
| mean anomaly at epoch: | 260.2116° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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