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 56078U 26145.31268892 +.00000000 +00000-0 +31237-3 0 00005
2 56078 87.8990 263.7729 0002214 104.2873 255.8504 13.15547509 08
| Epoch (UTC): | 25 May 2026 07:30:16 |
| Eccentricity: | 0.0002214 |
| inclination: | 87.8990° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7729° |
| argument of perigee: | 104.2873° |
| revolutions per day: | 13.15547509 |
| mean anomaly at epoch: | 255.8504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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