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 63579U 26145.33958872 +.00000000 +00000-0 +61718-3 0 00002
2 63579 43.0017 248.6820 0000317 39.8863 320.2012 15.27579071 09
| Epoch (UTC): | 25 May 2026 08:09:00 |
| Eccentricity: | 0.0000317 |
| inclination: | 43.0017° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 248.6820° |
| argument of perigee: | 39.8863° |
| revolutions per day: | 15.27579071 |
| mean anomaly at epoch: | 320.2012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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