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 65050U 26145.62898383 +.00000000 +00000-0 +77131-4 0 00007
2 65050 50.0043 346.4180 0000512 47.1621 312.9294 13.29323090 07
| Epoch (UTC): | 25 May 2026 15:05:44 |
| Eccentricity: | 0.0000512 |
| inclination: | 50.0043° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 346.4180° |
| argument of perigee: | 47.1621° |
| revolutions per day: | 13.29323090 |
| mean anomaly at epoch: | 312.9294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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