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 25544U 26137.87541122 +.00000000 +00000-0 +10059-3 0 00000
2 25544 51.6321 90.1533 0007579 69.9393 290.2410 15.49247594 06
| Epoch (UTC): | 17 May 2026 21:00:35 |
| Eccentricity: | 0.0007579 |
| inclination: | 51.6321° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 90.1533° |
| argument of perigee: | 69.9393° |
| revolutions per day: | 15.49247594 |
| mean anomaly at epoch: | 290.2410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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