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 59632U 26145.46799249 +.00000000 +00000-0 +73004-4 0 00004
2 59632 43.0060 52.0933 0001385 249.6829 110.3874 15.27572093 04
| Epoch (UTC): | 25 May 2026 11:13:54 |
| Eccentricity: | 0.0001385 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 52.0933° |
| argument of perigee: | 249.6829° |
| revolutions per day: | 15.27572093 |
| mean anomaly at epoch: | 110.3874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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