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 26065.78928795 +.00000000 +00000-0 +16182-3 0 00008
2 40376 98.1312 74.3184 0001321 112.5858 247.5484 14.63334850 01
| Epoch (UTC): | 06 March 2026 18:56:34 |
| Eccentricity: | 0.0001321 |
| inclination: | 98.1312° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 74.3184° |
| argument of perigee: | 112.5858° |
| revolutions per day: | 14.63334850 |
| mean anomaly at epoch: | 247.5484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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