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 56783U 26145.34432446 +.00000000 +00000-0 -35630-5 0 00003
2 56783 69.9986 131.2635 0003775 263.8523 96.2206 14.98330821 04
| Epoch (UTC): | 25 May 2026 08:15:49 |
| Eccentricity: | 0.0003775 |
| inclination: | 69.9986° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 131.2635° |
| argument of perigee: | 263.8523° |
| revolutions per day: | 14.98330821 |
| mean anomaly at epoch: | 96.2206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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