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 60561U 26145.48737933 +.00000000 +00000-0 +39361-3 0 00008
2 60561 97.3697 229.1949 0003987 32.4123 327.7368 15.40795473 00
| Epoch (UTC): | 25 May 2026 11:41:49 |
| Eccentricity: | 0.0003987 |
| inclination: | 97.3697° |
| perigee height: | 441 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 229.1949° |
| argument of perigee: | 32.4123° |
| revolutions per day: | 15.40795473 |
| mean anomaly at epoch: | 327.7368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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