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 56113U 26145.11459295 +.00000000 +00000-0 +14405-4 0 00001
2 56113 43.0064 89.6036 0001455 267.8548 92.2137 15.27572876 06
| Epoch (UTC): | 25 May 2026 02:45:00 |
| Eccentricity: | 0.0001455 |
| inclination: | 43.0064° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 89.6036° |
| argument of perigee: | 267.8548° |
| revolutions per day: | 15.27572876 |
| mean anomaly at epoch: | 92.2137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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