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 56883U 26145.32799476 +.00000000 +00000-0 +10229-3 0 00005
2 56883 43.0031 12.1762 0000901 249.8778 110.1976 15.27583076 06
| Epoch (UTC): | 25 May 2026 07:52:18 |
| Eccentricity: | 0.0000901 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.1762° |
| argument of perigee: | 249.8778° |
| revolutions per day: | 15.27583076 |
| mean anomaly at epoch: | 110.1976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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