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 65557U 26145.01572608 +.00000000 +00000-0 +17176-3 0 00003
2 65557 49.9778 142.9712 0002073 234.3835 125.6910 14.82768213 06
| Epoch (UTC): | 25 May 2026 00:22:38 |
| Eccentricity: | 0.0002073 |
| inclination: | 49.9778° |
| perigee height: | 619 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 142.9712° |
| argument of perigee: | 234.3835° |
| revolutions per day: | 14.82768213 |
| mean anomaly at epoch: | 125.6910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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