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 68591U 26145.36708826 +.00000000 +00000-0 +86404-3 0 00005
2 68591 51.8650 287.6855 0010850 312.1105 47.8958 15.36471553 05
| Epoch (UTC): | 25 May 2026 08:48:36 |
| Eccentricity: | 0.0010850 |
| inclination: | 51.8650° |
| perigee height: | 449 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 287.6855° |
| argument of perigee: | 312.1105° |
| revolutions per day: | 15.36471553 |
| mean anomaly at epoch: | 47.8958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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