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 66086U 26145.13079973 +.00000000 +00000-0 +14877-2 0 00005
2 66086 53.1576 109.1264 0001152 116.6570 243.4549 15.30239928 06
| Epoch (UTC): | 25 May 2026 03:08:21 |
| Eccentricity: | 0.0001152 |
| inclination: | 53.1576° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 109.1264° |
| argument of perigee: | 116.6570° |
| revolutions per day: | 15.30239928 |
| mean anomaly at epoch: | 243.4549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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