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 65589U 26144.00263696 +.00000000 +00000-0 +00000-0 0 00005
2 65589 64.6535 315.6878 0065807 305.4446 53.9403 2.14901283 08
| Epoch (UTC): | 24 May 2026 00:03:47 |
| Eccentricity: | 0.0065807 |
| inclination: | 64.6535° |
| perigee height: | 18820 km |
| apogee height: | 19154 km |
| right ascension of ascending node: | 315.6878° |
| argument of perigee: | 305.4446° |
| revolutions per day: | 2.14901283 |
| mean anomaly at epoch: | 53.9403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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