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 53906U 26144.96295500 +.00000000 +00000-0 +41541-4 0 00008
2 53906 53.2134 331.4336 0001407 68.8359 291.2784 15.08839917 01
| Epoch (UTC): | 24 May 2026 23:06:39 |
| Eccentricity: | 0.0001407 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 331.4336° |
| argument of perigee: | 68.8359° |
| revolutions per day: | 15.08839917 |
| mean anomaly at epoch: | 291.2784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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