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 56498U 26145.39600890 +.00000000 +00000-0 +22586-4 0 00005
2 56498 69.9991 270.9963 0002972 270.3519 89.7299 14.98329097 06
| Epoch (UTC): | 25 May 2026 09:30:15 |
| Eccentricity: | 0.0002972 |
| inclination: | 69.9991° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 270.9963° |
| argument of perigee: | 270.3519° |
| revolutions per day: | 14.98329097 |
| mean anomaly at epoch: | 89.7299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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