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 65105U 26145.39610065 +.00000000 +00000-0 +42506-3 0 00008
2 65105 53.1602 27.5407 0001413 94.1464 265.9704 15.42154960 08
| Epoch (UTC): | 25 May 2026 09:30:23 |
| Eccentricity: | 0.0001413 |
| inclination: | 53.1602° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 27.5407° |
| argument of perigee: | 94.1464° |
| revolutions per day: | 15.42154960 |
| mean anomaly at epoch: | 265.9704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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