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 65049U 26145.48698214 +.00000000 +00000-0 +67405-4 0 00003
2 65049 50.0079 347.0845 0000490 42.4376 317.6534 13.29323444 01
| Epoch (UTC): | 25 May 2026 11:41:15 |
| Eccentricity: | 0.0000490 |
| inclination: | 50.0079° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 347.0845° |
| argument of perigee: | 42.4376° |
| revolutions per day: | 13.29323444 |
| mean anomaly at epoch: | 317.6534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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