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 59956U 26144.73770549 +.00000000 +00000-0 +20018-4 0 00001
2 59956 53.1593 236.1182 0001192 91.4516 268.6639 15.69718331 08
| Epoch (UTC): | 24 May 2026 17:42:17 |
| Eccentricity: | 0.0001192 |
| inclination: | 53.1593° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 236.1182° |
| argument of perigee: | 91.4516° |
| revolutions per day: | 15.69718331 |
| mean anomaly at epoch: | 268.6639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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