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 26076.25104068 +.00000000 +00000-0 +10413-3 0 00002
2 40376 98.1311 84.6341 0001625 109.0949 251.0429 14.63348965 09
| Epoch (UTC): | 17 March 2026 06:01:29 |
| Eccentricity: | 0.0001625 |
| inclination: | 98.1311° |
| perigee height: | 681 km |
| apogee height: | 684 km |
| right ascension of ascending node: | 84.6341° |
| argument of perigee: | 109.0949° |
| revolutions per day: | 14.63348965 |
| mean anomaly at epoch: | 251.0429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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