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 26042.26719685 +.00000000 +00000-0 +13428-3 0 00002
2 40376 98.1306 51.1277 0001451 89.1490 270.9878 14.63442434 00
| Epoch (UTC): | 11 February 2026 06:24:45 |
| Eccentricity: | 0.0001451 |
| inclination: | 98.1306° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 51.1277° |
| argument of perigee: | 89.1490° |
| revolutions per day: | 14.63442434 |
| mean anomaly at epoch: | 270.9878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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