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 25544U 26158.32089647 +.00000000 +00000-0 +16649-3 0 00003
2 25544 51.6340 348.9335 0006961 143.5924 216.5539 15.49651405 07
| Epoch (UTC): | 07 June 2026 07:42:05 |
| Eccentricity: | 0.0006961 |
| inclination: | 51.6340° |
| perigee height: | 413 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 348.9335° |
| argument of perigee: | 143.5924° |
| revolutions per day: | 15.49651405 |
| mean anomaly at epoch: | 216.5539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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