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 56359U 26145.27796527 +.00000000 +00000-0 -15367-3 0 00000
2 56359 97.4453 145.1629 0002901 98.6181 261.5375 15.05658810 03
| Epoch (UTC): | 25 May 2026 06:40:16 |
| Eccentricity: | 0.0002901 |
| inclination: | 97.4453° |
| perigee height: | 547 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.1629° |
| argument of perigee: | 98.6181° |
| revolutions per day: | 15.05658810 |
| mean anomaly at epoch: | 261.5375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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