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 47770U 26145.44535330 +.00000000 +00000-0 +16851-5 0 00009
2 47770 53.1584 206.9217 0001277 83.3885 276.7262 15.31700786 02
| Epoch (UTC): | 25 May 2026 10:41:18 |
| Eccentricity: | 0.0001277 |
| inclination: | 53.1584° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 206.9217° |
| argument of perigee: | 83.3885° |
| revolutions per day: | 15.31700786 |
| mean anomaly at epoch: | 276.7262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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