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 31114U 26139.88041558 +.00000000 +00000-0 +44960-4 0 00000
2 31114 98.4070 249.6204 0060184 87.4211 273.3854 14.20268618 09
| Epoch (UTC): | 19 May 2026 21:07:47 |
| Eccentricity: | 0.0060184 |
| inclination: | 98.4070° |
| perigee height: | 781 km |
| apogee height: | 868 km |
| right ascension of ascending node: | 249.6204° |
| argument of perigee: | 87.4211° |
| revolutions per day: | 14.20268618 |
| mean anomaly at epoch: | 273.3854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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