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 26066.47492980 +.00000000 +00000-0 +29891-3 0 00000
2 40071 98.3761 22.1027 0005904 239.2239 120.8396 14.89608671 09
| Epoch (UTC): | 07 March 2026 11:23:53 |
| Eccentricity: | 0.0005904 |
| inclination: | 98.3761° |
| perigee height: | 595 km |
| apogee height: | 603 km |
| right ascension of ascending node: | 22.1027° |
| argument of perigee: | 239.2239° |
| revolutions per day: | 14.89608671 |
| mean anomaly at epoch: | 120.8396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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