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 56418U 26144.94437056 +.00000000 +00000-0 +52737-3 0 00009
2 56418 43.0035 108.7526 0001122 263.1490 96.9234 15.27548263 07
| Epoch (UTC): | 24 May 2026 22:39:53 |
| Eccentricity: | 0.0001122 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 108.7526° |
| argument of perigee: | 263.1490° |
| revolutions per day: | 15.27548263 |
| mean anomaly at epoch: | 96.9234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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