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 55577U 26145.41111264 +.00000000 +00000-0 +95384-3 0 00002
2 55577 43.0017 292.0756 0002549 274.3810 85.6750 15.27520425 06
| Epoch (UTC): | 25 May 2026 09:52:00 |
| Eccentricity: | 0.0002549 |
| inclination: | 43.0017° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 292.0756° |
| argument of perigee: | 274.3810° |
| revolutions per day: | 15.27520425 |
| mean anomaly at epoch: | 85.6750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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