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 40376U 26062.98579233 +.00000000 +00000-0 +16690-3 0 00000
2 40376 98.1310 71.5542 0001242 112.9009 247.2324 14.63330660 05
| Epoch (UTC): | 03 March 2026 23:39:32 |
| Eccentricity: | 0.0001242 |
| inclination: | 98.1310° |
| perigee height: | 682 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 71.5542° |
| argument of perigee: | 112.9009° |
| revolutions per day: | 14.63330660 |
| mean anomaly at epoch: | 247.2324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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