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 66208U 26145.51184913 +.00000000 +00000-0 +50483-3 0 00008
2 66208 53.1586 232.9173 0001385 86.0426 274.0733 15.30205789 08
| Epoch (UTC): | 25 May 2026 12:17:03 |
| Eccentricity: | 0.0001385 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.9173° |
| argument of perigee: | 86.0426° |
| revolutions per day: | 15.30205789 |
| mean anomaly at epoch: | 274.0733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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