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 26073.58432875 +.00000000 +00000-0 +13404-3 0 00008
2 40376 98.1311 82.0045 0001543 109.6243 250.5125 14.63346391 02
| Epoch (UTC): | 14 March 2026 14:01:26 |
| Eccentricity: | 0.0001543 |
| inclination: | 98.1311° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 82.0045° |
| argument of perigee: | 109.6243° |
| revolutions per day: | 14.63346391 |
| mean anomaly at epoch: | 250.5125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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