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 39440U 26162.30229726 +.00000000 +00000-0 +29203-3 0 00000
2 39440 97.8900 111.2555 0058933 48.0727 312.5496 14.93713369 07
| Epoch (UTC): | 11 June 2026 07:15:18 |
| Eccentricity: | 0.0058933 |
| inclination: | 97.8900° |
| perigee height: | 545 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 111.2555° |
| argument of perigee: | 48.0727° |
| revolutions per day: | 14.93713369 |
| mean anomaly at epoch: | 312.5496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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