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 26069.55006110 +.00000000 +00000-0 +14217-3 0 00002
2 40376 98.1313 78.0266 0001440 111.4120 248.7235 14.63340404 05
| Epoch (UTC): | 10 March 2026 13:12:05 |
| Eccentricity: | 0.0001440 |
| inclination: | 98.1313° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 78.0266° |
| argument of perigee: | 111.4120° |
| revolutions per day: | 14.63340404 |
| mean anomaly at epoch: | 248.7235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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