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 39522U 26145.59204846 +.00000000 +00000-0 +00000-0 0 00000
2 39522 0.0445 297.6199 0001863 36.7297 163.9504 1.00270657 07
| Epoch (UTC): | 25 May 2026 14:12:32 |
| Eccentricity: | 0.0001863 |
| inclination: | 0.0445° |
| perigee height: | 35779 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 297.6199° |
| argument of perigee: | 36.7297° |
| revolutions per day: | 1.00270657 |
| mean anomaly at epoch: | 163.9504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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