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 62911U 26145.63759294 +.00000000 +00000-0 +13964-2 0 00000
2 62911 43.0041 243.8814 0002244 277.9657 82.0956 15.70863494 05
| Epoch (UTC): | 25 May 2026 15:18:08 |
| Eccentricity: | 0.0002244 |
| inclination: | 43.0041° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 243.8814° |
| argument of perigee: | 277.9657° |
| revolutions per day: | 15.70863494 |
| mean anomaly at epoch: | 82.0956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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