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 40071U 26108.58920189 +.00000000 +00000-0 +81902-4 0 00008
2 40071 98.3825 66.7027 0008588 102.2833 257.9345 14.89792242 08
| Epoch (UTC): | 18 April 2026 14:08:27 |
| Eccentricity: | 0.0008588 |
| inclination: | 98.3825° |
| perigee height: | 593 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 66.7027° |
| argument of perigee: | 102.2833° |
| revolutions per day: | 14.89792242 |
| mean anomaly at epoch: | 257.9345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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