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 63582U 26145.58571926 +.00000000 +00000-0 +67921-3 0 00006
2 63582 43.0004 247.1677 0000964 286.5351 73.5395 15.27596114 03
| Epoch (UTC): | 25 May 2026 14:03:26 |
| Eccentricity: | 0.0000964 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.1677° |
| argument of perigee: | 286.5351° |
| revolutions per day: | 15.27596114 |
| mean anomaly at epoch: | 73.5395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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