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 26041.92533299 +.00000000 +00000-0 +12939-3 0 00005
2 40376 98.1306 50.7907 0001458 88.9142 271.2227 14.63441748 02
| Epoch (UTC): | 10 February 2026 22:12:28 |
| Eccentricity: | 0.0001458 |
| inclination: | 98.1306° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 50.7907° |
| argument of perigee: | 88.9142° |
| revolutions per day: | 14.63441748 |
| mean anomaly at epoch: | 271.2227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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