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 51770U 26144.99195803 +.00000000 +00000-0 -34170-3 0 00003
2 51770 53.2149 356.5856 0001407 94.1559 265.9594 15.08869979 01
| Epoch (UTC): | 24 May 2026 23:48:25 |
| Eccentricity: | 0.0001407 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 356.5856° |
| argument of perigee: | 94.1559° |
| revolutions per day: | 15.08869979 |
| mean anomaly at epoch: | 265.9594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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