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 26108.78021580 +.00000000 +00000-0 +15594-3 0 00008
2 25544 51.6329 234.1171 0006603 323.1571 36.8962 15.48819285 09
| Epoch (UTC): | 18 April 2026 18:43:30 |
| Eccentricity: | 0.0006603 |
| inclination: | 51.6329° |
| perigee height: | 416 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 234.1171° |
| argument of perigee: | 323.1571° |
| revolutions per day: | 15.48819285 |
| mean anomaly at epoch: | 36.8962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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