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 56484U 26145.34616933 +.00000000 +00000-0 +27739-4 0 00005
2 56484 69.9987 291.0945 0003106 266.9896 93.0908 14.98330706 03
| Epoch (UTC): | 25 May 2026 08:18:29 |
| Eccentricity: | 0.0003106 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 291.0945° |
| argument of perigee: | 266.9896° |
| revolutions per day: | 14.98330706 |
| mean anomaly at epoch: | 93.0908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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