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 61541U 26145.41490185 +.00000000 +00000-0 -10046-5 0 00007
2 61541 53.1589 218.3419 0000850 60.8381 299.2722 15.69694329 04
| Epoch (UTC): | 25 May 2026 09:57:27 |
| Eccentricity: | 0.0000850 |
| inclination: | 53.1589° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 218.3419° |
| argument of perigee: | 60.8381° |
| revolutions per day: | 15.69694329 |
| mean anomaly at epoch: | 299.2722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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