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 26154.33051699 +.00000000 +00000-0 +47123-3 0 00007
2 39440 97.8904 103.2522 0059453 73.9566 286.8190 14.93641817 04
| Epoch (UTC): | 03 June 2026 07:55:56 |
| Eccentricity: | 0.0059453 |
| inclination: | 97.8904° |
| perigee height: | 545 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 103.2522° |
| argument of perigee: | 73.9566° |
| revolutions per day: | 14.93641817 |
| mean anomaly at epoch: | 286.8190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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