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 data is extracted from the following two-line orbital elements,
1 31114U 07010B 25188.19636770 .00000081 00000-0 56308-4 0 9996
2 31114 98.3818 308.9847 0057905 288.4323 71.0565 14.20134602944873
| Epoch (UTC): | 07 July 2025 04:42:46 |
| Eccentricity: | 0.0057905 |
| inclination: | 98.3818° |
| perigee height: | 783 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 308.9847° |
| argument of perigee: | 288.4323° |
| revolutions per day: | 14.20134602 |
| mean anomaly at epoch: | 71.0565° |
| orbit number at epoch: | 94487 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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