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 26067.08846578 +.00000000 +00000-0 +16668-3 0 00000
2 40376 98.1313 75.5994 0001366 112.5920 247.5427 14.63337133 07
| Epoch (UTC): | 08 March 2026 02:07:23 |
| Eccentricity: | 0.0001366 |
| inclination: | 98.1313° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 75.5994° |
| argument of perigee: | 112.5920° |
| revolutions per day: | 14.63337133 |
| mean anomaly at epoch: | 247.5427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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