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 53590U 26145.66668980 +.00000000 +00000-0 +10108-1 0 00003
2 53590 53.2249 252.3555 0001455 73.7099 321.1793 15.43787464 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001455 |
| inclination: | 53.2249° |
| perigee height: | 434 km |
| apogee height: | 436 km |
| right ascension of ascending node: | 252.3555° |
| argument of perigee: | 73.7099° |
| revolutions per day: | 15.43787464 |
| mean anomaly at epoch: | 321.1793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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