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 26109.26084285 +.00000000 +00000-0 +93092-4 0 00005
2 40071 98.3827 67.4149 0008584 100.4868 259.7315 14.89793937 06
| Epoch (UTC): | 19 April 2026 06:15:36 |
| Eccentricity: | 0.0008584 |
| inclination: | 98.3827° |
| perigee height: | 593 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 67.4149° |
| argument of perigee: | 100.4868° |
| revolutions per day: | 14.89793937 |
| mean anomaly at epoch: | 259.7315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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