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 26070.84923376 +.00000000 +00000-0 +12644-3 0 00000
2 40376 98.1312 79.3076 0001475 111.0393 249.0967 14.63342048 05
| Epoch (UTC): | 11 March 2026 20:22:53 |
| Eccentricity: | 0.0001475 |
| inclination: | 98.1312° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 79.3076° |
| argument of perigee: | 111.0393° |
| revolutions per day: | 14.63342048 |
| mean anomaly at epoch: | 249.0967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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