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 55451U 26145.03358455 +.00000000 +00000-0 +87404-4 0 00001
2 55451 43.0040 257.9392 0001864 285.8720 74.1926 15.27589781 03
| Epoch (UTC): | 25 May 2026 00:48:21 |
| Eccentricity: | 0.0001864 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 257.9392° |
| argument of perigee: | 285.8720° |
| revolutions per day: | 15.27589781 |
| mean anomaly at epoch: | 74.1926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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