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 26075.27436124 +.00000000 +00000-0 +28132-3 0 00003
2 40071 98.3760 31.4168 0006385 206.3808 153.7084 14.89657955 06
| Epoch (UTC): | 16 March 2026 06:35:04 |
| Eccentricity: | 0.0006385 |
| inclination: | 98.3760° |
| perigee height: | 595 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 31.4168° |
| argument of perigee: | 206.3808° |
| revolutions per day: | 14.89657955 |
| mean anomaly at epoch: | 153.7084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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