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 65217U 26145.44050956 +.00000000 +00000-0 +45479-3 0 00007
2 65217 53.1592 155.3580 0001203 81.7833 278.3306 15.34405967 04
| Epoch (UTC): | 25 May 2026 10:34:20 |
| Eccentricity: | 0.0001203 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 155.3580° |
| argument of perigee: | 81.7833° |
| revolutions per day: | 15.34405967 |
| mean anomaly at epoch: | 278.3306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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