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 61055U 26145.41848455 +.00000000 +00000-0 +78987-5 0 00001
2 61055 53.1578 292.7560 0000760 35.8687 324.2382 15.69708374 03
| Epoch (UTC): | 25 May 2026 10:02:37 |
| Eccentricity: | 0.0000760 |
| inclination: | 53.1578° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 292.7560° |
| argument of perigee: | 35.8687° |
| revolutions per day: | 15.69708374 |
| mean anomaly at epoch: | 324.2382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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