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 66108U 26145.09701786 +.00000000 +00000-0 +43702-3 0 00009
2 66108 53.1597 108.9066 0001301 107.3165 252.7979 15.30210017 02
| Epoch (UTC): | 25 May 2026 02:19:42 |
| Eccentricity: | 0.0001301 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.9066° |
| argument of perigee: | 107.3165° |
| revolutions per day: | 15.30210017 |
| mean anomaly at epoch: | 252.7979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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