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 65109U 26145.65746073 +.00000000 +00000-0 +94152-4 0 00005
2 65109 50.0043 46.5432 0010688 34.1977 325.9582 13.29318308 05
| Epoch (UTC): | 25 May 2026 15:46:44 |
| Eccentricity: | 0.0010688 |
| inclination: | 50.0043° |
| perigee height: | 1141 km |
| apogee height: | 1157 km |
| right ascension of ascending node: | 46.5432° |
| argument of perigee: | 34.1977° |
| revolutions per day: | 13.29318308 |
| mean anomaly at epoch: | 325.9582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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