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 65112U 26145.64067502 +.00000000 +00000-0 +98908-4 0 00004
2 65112 50.0007 46.3732 0012194 26.1544 333.9942 13.29318275 07
| Epoch (UTC): | 25 May 2026 15:22:34 |
| Eccentricity: | 0.0012194 |
| inclination: | 50.0007° |
| perigee height: | 1140 km |
| apogee height: | 1159 km |
| right ascension of ascending node: | 46.3732° |
| argument of perigee: | 26.1544° |
| revolutions per day: | 13.29318275 |
| mean anomaly at epoch: | 333.9942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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