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 59578U 26145.43237492 +.00000000 +00000-0 +18946-3 0 00000
2 59578 42.9984 295.2350 0000923 282.4254 77.6494 15.27587496 00
| Epoch (UTC): | 25 May 2026 10:22:37 |
| Eccentricity: | 0.0000923 |
| inclination: | 42.9984° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.2350° |
| argument of perigee: | 282.4254° |
| revolutions per day: | 15.27587496 |
| mean anomaly at epoch: | 77.6494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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