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 26071.19112105 +.00000000 +00000-0 +14063-3 0 00006
2 40376 98.1312 79.6447 0001486 110.9968 249.1393 14.63342961 06
| Epoch (UTC): | 12 March 2026 04:35:12 |
| Eccentricity: | 0.0001486 |
| inclination: | 98.1312° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 79.6447° |
| argument of perigee: | 110.9968° |
| revolutions per day: | 14.63342961 |
| mean anomaly at epoch: | 249.1393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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