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 66485U 26145.39745970 +.00000000 +00000-0 +78110-3 0 00004
2 66485 42.9967 277.2137 0000680 291.9391 68.1388 15.27597226 05
| Epoch (UTC): | 25 May 2026 09:32:20 |
| Eccentricity: | 0.0000680 |
| inclination: | 42.9967° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 277.2137° |
| argument of perigee: | 291.9391° |
| revolutions per day: | 15.27597226 |
| mean anomaly at epoch: | 68.1388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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