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 65590U 26140.53574256 +.00000000 +00000-0 +00000-0 0 00008
2 65590 64.6521 315.9473 0011199 315.4946 223.7566 2.13100430 01
| Epoch (UTC): | 20 May 2026 12:51:28 |
| Eccentricity: | 0.0011199 |
| inclination: | 64.6521° |
| perigee height: | 19101 km |
| apogee height: | 19159 km |
| right ascension of ascending node: | 315.9473° |
| argument of perigee: | 315.4946° |
| revolutions per day: | 2.13100430 |
| mean anomaly at epoch: | 223.7566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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