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 26159.82371896 +.00000000 +00000-0 +37815-3 0 00007
2 39440 97.8903 108.7669 0059218 56.2091 304.4748 14.93696969 05
| Epoch (UTC): | 08 June 2026 19:46:09 |
| Eccentricity: | 0.0059218 |
| inclination: | 97.8903° |
| perigee height: | 545 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 108.7669° |
| argument of perigee: | 56.2091° |
| revolutions per day: | 14.93696969 |
| mean anomaly at epoch: | 304.4748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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