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 53909U 26144.94831123 +.00000000 +00000-0 +18589-5 0 00003
2 53909 53.2122 332.0427 0001358 86.4703 273.6444 15.08829450 01
| Epoch (UTC): | 24 May 2026 22:45:34 |
| Eccentricity: | 0.0001358 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 332.0427° |
| argument of perigee: | 86.4703° |
| revolutions per day: | 15.08829450 |
| mean anomaly at epoch: | 273.6444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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