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 66065U 26145.54679370 +.00000000 +00000-0 +30046-3 0 00001
2 66065 53.1608 248.6308 0000279 51.0948 309.0077 15.30201673 08
| Epoch (UTC): | 25 May 2026 13:07:22 |
| Eccentricity: | 0.0000279 |
| inclination: | 53.1608° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 248.6308° |
| argument of perigee: | 51.0948° |
| revolutions per day: | 15.30201673 |
| mean anomaly at epoch: | 309.0077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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