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 26150.50707608 +.00000000 +00000-0 +12037-3 0 00006
2 40376 98.1277 157.8524 0001258 89.0495 271.0851 14.63349125 01
| Epoch (UTC): | 30 May 2026 12:10:11 |
| Eccentricity: | 0.0001258 |
| inclination: | 98.1277° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 157.8524° |
| argument of perigee: | 89.0495° |
| revolutions per day: | 14.63349125 |
| mean anomaly at epoch: | 271.0851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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