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 65611U 26145.42669780 +.00000000 +00000-0 +34952-3 0 00008
2 65611 97.4461 213.8625 0002174 118.6230 241.5216 15.05658680 09
| Epoch (UTC): | 25 May 2026 10:14:26 |
| Eccentricity: | 0.0002174 |
| inclination: | 97.4461° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 213.8625° |
| argument of perigee: | 118.6230° |
| revolutions per day: | 15.05658680 |
| mean anomaly at epoch: | 241.5216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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