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 40339U 26145.60008264 +.00000000 +00000-0 +19857-3 0 00009
2 40339 63.3906 9.1050 0364940 8.8562 351.8673 13.45433608 08
| Epoch (UTC): | 25 May 2026 14:24:07 |
| Eccentricity: | 0.0364940 |
| inclination: | 63.3906° |
| perigee height: | 817 km |
| apogee height: | 1362 km |
| right ascension of ascending node: | 9.1050° |
| argument of perigee: | 8.8562° |
| revolutions per day: | 13.45433608 |
| mean anomaly at epoch: | 351.8673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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