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 26066.13117725 +.00000000 +00000-0 +14190-3 0 00008
2 40376 98.1313 74.6555 0001328 112.4520 247.6823 14.63334773 01
| Epoch (UTC): | 07 March 2026 03:08:53 |
| Eccentricity: | 0.0001328 |
| inclination: | 98.1313° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 74.6555° |
| argument of perigee: | 112.4520° |
| revolutions per day: | 14.63334773 |
| mean anomaly at epoch: | 247.6823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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