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 66935U 26145.62322359 +.00000000 +00000-0 +65605-3 0 00007
2 66935 53.1603 0.5391 0001318 97.9103 262.2050 15.34406917 06
| Epoch (UTC): | 25 May 2026 14:57:26 |
| Eccentricity: | 0.0001318 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 0.5391° |
| argument of perigee: | 97.9103° |
| revolutions per day: | 15.34406917 |
| mean anomaly at epoch: | 262.2050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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