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 56844U 26144.96887309 +.00000000 +00000-0 -80912-4 0 00002
2 56844 43.0063 36.2103 0000999 214.5157 145.5630 15.27590345 07
| Epoch (UTC): | 24 May 2026 23:15:10 |
| Eccentricity: | 0.0000999 |
| inclination: | 43.0063° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 36.2103° |
| argument of perigee: | 214.5157° |
| revolutions per day: | 15.27590345 |
| mean anomaly at epoch: | 145.5630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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