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 65113U 26145.63238910 +.00000000 +00000-0 +11481-3 0 00007
2 65113 49.9999 46.3093 0012077 45.5654 314.6205 13.29317673 01
| Epoch (UTC): | 25 May 2026 15:10:38 |
| Eccentricity: | 0.0012077 |
| inclination: | 49.9999° |
| perigee height: | 1140 km |
| apogee height: | 1158 km |
| right ascension of ascending node: | 46.3093° |
| argument of perigee: | 45.5654° |
| revolutions per day: | 13.29317673 |
| mean anomaly at epoch: | 314.6205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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