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 57528U 26145.43596863 +.00000000 +00000-0 +14036-4 0 00000
2 57528 43.0040 288.6240 0001450 273.1010 86.9676 15.27571308 05
| Epoch (UTC): | 25 May 2026 10:27:47 |
| Eccentricity: | 0.0001450 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 288.6240° |
| argument of perigee: | 273.1010° |
| revolutions per day: | 15.27571308 |
| mean anomaly at epoch: | 86.9676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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