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 53936U 26145.55865889 +.00000000 +00000-0 +22033-4 0 00005
2 53936 53.2124 313.7755 0001198 96.6240 263.4889 15.08835447 07
| Epoch (UTC): | 25 May 2026 13:24:28 |
| Eccentricity: | 0.0001198 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 313.7755° |
| argument of perigee: | 96.6240° |
| revolutions per day: | 15.08835447 |
| mean anomaly at epoch: | 263.4889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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