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 56000U 26145.60680644 +.00000000 +00000-0 +24899-4 0 00002
2 56000 43.0052 345.1501 0001426 273.4107 86.6582 15.27575768 01
| Epoch (UTC): | 25 May 2026 14:33:48 |
| Eccentricity: | 0.0001426 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.1501° |
| argument of perigee: | 273.4107° |
| revolutions per day: | 15.27575768 |
| mean anomaly at epoch: | 86.6582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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