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 56360U 26144.95809825 +.00000000 +00000-0 +79307-4 0 00006
2 56360 97.4508 146.0443 0001579 76.1869 283.9534 15.05654714 08
| Epoch (UTC): | 24 May 2026 22:59:39 |
| Eccentricity: | 0.0001579 |
| inclination: | 97.4508° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.0443° |
| argument of perigee: | 76.1869° |
| revolutions per day: | 15.05654714 |
| mean anomaly at epoch: | 283.9534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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