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 55364U 26145.58367144 +.00000000 +00000-0 +44610-4 0 00001
2 55364 43.0023 232.5345 0001538 263.7160 96.3517 15.27577033 04
| Epoch (UTC): | 25 May 2026 14:00:29 |
| Eccentricity: | 0.0001538 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 232.5345° |
| argument of perigee: | 263.7160° |
| revolutions per day: | 15.27577033 |
| mean anomaly at epoch: | 96.3517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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