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 59154U 26145.38171758 +.00000000 +00000-0 +14336-3 0 00005
2 59154 43.0025 33.9983 0001530 265.9064 94.1613 15.27593553 05
| Epoch (UTC): | 25 May 2026 09:09:40 |
| Eccentricity: | 0.0001530 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.9983° |
| argument of perigee: | 265.9064° |
| revolutions per day: | 15.27593553 |
| mean anomaly at epoch: | 94.1613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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