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 65108U 26145.66562757 +.00000000 +00000-0 +80264-4 0 00009
2 65108 50.0049 46.6072 0010636 21.9341 338.1985 13.29320351 07
| Epoch (UTC): | 25 May 2026 15:58:30 |
| Eccentricity: | 0.0010636 |
| inclination: | 50.0049° |
| perigee height: | 1141 km |
| apogee height: | 1157 km |
| right ascension of ascending node: | 46.6072° |
| argument of perigee: | 21.9341° |
| revolutions per day: | 13.29320351 |
| mean anomaly at epoch: | 338.1985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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