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 40047U 26156.36291779 +.00000000 +00000-0 +18666-4 0 00003
2 40047 97.8690 17.1423 0566731 322.2067 34.0519 13.61963895 07
| Epoch (UTC): | 05 June 2026 08:42:36 |
| Eccentricity: | 0.0566731 |
| inclination: | 97.8690° |
| perigee height: | 609 km |
| apogee height: | 1448 km |
| right ascension of ascending node: | 17.1423° |
| argument of perigee: | 322.2067° |
| revolutions per day: | 13.61963895 |
| mean anomaly at epoch: | 34.0519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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