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 28526U 26145.28703611 +.00000000 +00000-0 +00000-0 0 00002
2 28526 6.3949 70.7296 0003041 347.8650 250.1605 1.00271640 08
| Epoch (UTC): | 25 May 2026 06:53:19 |
| Eccentricity: | 0.0003041 |
| inclination: | 6.3949° |
| perigee height: | 35774 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 70.7296° |
| argument of perigee: | 347.8650° |
| revolutions per day: | 1.00271640 |
| mean anomaly at epoch: | 250.1605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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