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 56544U 26145.36974203 +.00000000 +00000-0 +19257-4 0 00007
2 56544 43.0006 150.1791 0001127 268.9961 91.0762 15.27575895 04
| Epoch (UTC): | 25 May 2026 08:52:25 |
| Eccentricity: | 0.0001127 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.1791° |
| argument of perigee: | 268.9961° |
| revolutions per day: | 15.27575895 |
| mean anomaly at epoch: | 91.0762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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