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 40081U 26145.49129269 +.00000000 +00000-0 +00000-0 0 00006
2 40081 0.0491 351.3043 0002634 70.7446 297.9774 5.00115729 06
| Epoch (UTC): | 25 May 2026 11:47:27 |
| Eccentricity: | 0.0002634 |
| inclination: | 0.0491° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 351.3043° |
| argument of perigee: | 70.7446° |
| revolutions per day: | 5.00115729 |
| mean anomaly at epoch: | 297.9774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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