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 26154.13105986 +.00000000 +00000-0 +10833-3 0 00002
2 40376 98.1276 161.4248 0001260 90.9928 269.1418 14.63353401 08
| Epoch (UTC): | 03 June 2026 03:08:43 |
| Eccentricity: | 0.0001260 |
| inclination: | 98.1276° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 161.4248° |
| argument of perigee: | 90.9928° |
| revolutions per day: | 14.63353401 |
| mean anomaly at epoch: | 269.1418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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