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 56124U 26145.48829044 +.00000000 +00000-0 +20416-4 0 00005
2 56124 43.0035 73.4313 0000968 245.6193 114.4558 15.27576444 02
| Epoch (UTC): | 25 May 2026 11:43:08 |
| Eccentricity: | 0.0000968 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 73.4313° |
| argument of perigee: | 245.6193° |
| revolutions per day: | 15.27576444 |
| mean anomaly at epoch: | 114.4558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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