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 66817U 26145.41158463 +.00000000 +00000-0 +85613-3 0 00007
2 66817 43.0027 40.9989 0001716 273.3988 86.6668 15.27563992 09
| Epoch (UTC): | 25 May 2026 09:52:40 |
| Eccentricity: | 0.0001716 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 40.9989° |
| argument of perigee: | 273.3988° |
| revolutions per day: | 15.27563992 |
| mean anomaly at epoch: | 86.6668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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