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 31118U 26032.45397993 +.00000000 +00000-0 +80360-4 0 00000
2 31118 98.1296 342.9066 0013491 302.4136 57.5765 14.71315748 04
| Epoch (UTC): | 01 February 2026 10:53:43 |
| Eccentricity: | 0.0013491 |
| inclination: | 98.1296° |
| perigee height: | 647 km |
| apogee height: | 666 km |
| right ascension of ascending node: | 342.9066° |
| argument of perigee: | 302.4136° |
| revolutions per day: | 14.71315748 |
| mean anomaly at epoch: | 57.5765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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