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 26064.14821837 +.00000000 +00000-0 +15314-3 0 00002
2 40376 98.1311 72.7004 0001275 112.8388 247.2948 14.63332040 03
| Epoch (UTC): | 05 March 2026 03:33:26 |
| Eccentricity: | 0.0001275 |
| inclination: | 98.1311° |
| perigee height: | 682 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 72.7004° |
| argument of perigee: | 112.8388° |
| revolutions per day: | 14.63332040 |
| mean anomaly at epoch: | 247.2948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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