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 46567U 26145.58335647 +.00000000 +00000-0 +65876-3 0 00005
2 46567 53.0356 96.3383 0008451 75.4914 259.6142 15.81520902 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0008451 |
| inclination: | 53.0356° |
| perigee height: | 320 km |
| apogee height: | 332 km |
| right ascension of ascending node: | 96.3383° |
| argument of perigee: | 75.4914° |
| revolutions per day: | 15.81520902 |
| mean anomaly at epoch: | 259.6142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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