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 66415U 26145.34259171 +.00000000 +00000-0 +80682-4 0 00003
2 66415 50.0065 17.4973 0000981 60.5873 299.5097 13.29322898 06
| Epoch (UTC): | 25 May 2026 08:13:19 |
| Eccentricity: | 0.0000981 |
| inclination: | 50.0065° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 17.4973° |
| argument of perigee: | 60.5873° |
| revolutions per day: | 13.29322898 |
| mean anomaly at epoch: | 299.5097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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