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 26019.26964862 +.00000000 +00000-0 +66023-4 0 00005
2 31114 98.3971 135.0319 0060055 78.2174 282.5732 14.20225698 04
| Epoch (UTC): | 19 January 2026 06:28:17 |
| Eccentricity: | 0.0060055 |
| inclination: | 98.3971° |
| perigee height: | 781 km |
| apogee height: | 868 km |
| right ascension of ascending node: | 135.0319° |
| argument of perigee: | 78.2174° |
| revolutions per day: | 14.20225698 |
| mean anomaly at epoch: | 282.5732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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