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 47778U 26145.34407333 +.00000000 +00000-0 +10759-2 0 00005
2 47778 53.1582 201.6923 0005966 341.1176 18.9610 15.47039901 05
| Epoch (UTC): | 25 May 2026 08:15:27 |
| Eccentricity: | 0.0005966 |
| inclination: | 53.1582° |
| perigee height: | 421 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 201.6923° |
| argument of perigee: | 341.1176° |
| revolutions per day: | 15.47039901 |
| mean anomaly at epoch: | 18.9610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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