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 59392U 26145.30651076 +.00000000 +00000-0 +10776-3 0 00001
2 59392 53.1610 259.6529 0001248 97.0570 263.0573 15.30190308 03
| Epoch (UTC): | 25 May 2026 07:21:22 |
| Eccentricity: | 0.0001248 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 259.6529° |
| argument of perigee: | 97.0570° |
| revolutions per day: | 15.30190308 |
| mean anomaly at epoch: | 263.0573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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