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 56018U 26144.93817094 +.00000000 +00000-0 +36108-4 0 00003
2 56018 43.0021 334.8744 0001595 254.2430 105.8246 15.27577794 05
| Epoch (UTC): | 24 May 2026 22:30:57 |
| Eccentricity: | 0.0001595 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 334.8744° |
| argument of perigee: | 254.2430° |
| revolutions per day: | 15.27577794 |
| mean anomaly at epoch: | 105.8246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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