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 61947U 26145.00713168 +.00000000 +00000-0 +11985-2 0 00000
2 61947 53.1576 355.1051 0001529 38.5382 321.5745 15.69758553 03
| Epoch (UTC): | 25 May 2026 00:10:16 |
| Eccentricity: | 0.0001529 |
| inclination: | 53.1576° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 355.1051° |
| argument of perigee: | 38.5382° |
| revolutions per day: | 15.69758553 |
| mean anomaly at epoch: | 321.5745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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