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 66755U 26145.59847443 +.00000000 +00000-0 +12010-3 0 00001
2 66755 97.4208 218.5155 0003949 87.1324 273.0357 15.09918722 09
| Epoch (UTC): | 25 May 2026 14:21:48 |
| Eccentricity: | 0.0003949 |
| inclination: | 97.4208° |
| perigee height: | 534 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 218.5155° |
| argument of perigee: | 87.1324° |
| revolutions per day: | 15.09918722 |
| mean anomaly at epoch: | 273.0357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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