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 26067.01230808 +.00000000 +00000-0 +25785-3 0 00008
2 40071 98.3763 22.6715 0005956 236.3575 123.7073 14.89612591 08
| Epoch (UTC): | 08 March 2026 00:17:43 |
| Eccentricity: | 0.0005956 |
| inclination: | 98.3763° |
| perigee height: | 595 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 22.6715° |
| argument of perigee: | 236.3575° |
| revolutions per day: | 14.89612591 |
| mean anomaly at epoch: | 123.7073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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