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 31119U 26145.38584425 +.00000000 +00000-0 +87658-4 0 00003
2 31119 98.3766 119.0529 0054359 267.9683 91.5294 14.66083408 00
| Epoch (UTC): | 25 May 2026 09:15:36 |
| Eccentricity: | 0.0054359 |
| inclination: | 98.3766° |
| perigee height: | 635 km |
| apogee height: | 712 km |
| right ascension of ascending node: | 119.0529° |
| argument of perigee: | 267.9683° |
| revolutions per day: | 14.66083408 |
| mean anomaly at epoch: | 91.5294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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