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 26067.97737588 +.00000000 +00000-0 +15167-3 0 00001
2 40376 98.1313 76.4759 0001394 112.4217 247.7133 14.63338177 00
| Epoch (UTC): | 08 March 2026 23:27:25 |
| Eccentricity: | 0.0001394 |
| inclination: | 98.1313° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 76.4759° |
| argument of perigee: | 112.4217° |
| revolutions per day: | 14.63338177 |
| mean anomaly at epoch: | 247.7133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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