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 25198.34201200 .00000085 00000-0 58192-4 0 9997
2 31114 98.3828 318.5999 0057914 258.3100 101.1575 14.20136851946313
| Epoch (UTC): | 17 July 2025 08:12:29 |
| Eccentricity: | 0.0057914 |
| inclination: | 98.3828° |
| perigee height: | 783 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 318.5999° |
| argument of perigee: | 258.3100° |
| revolutions per day: | 14.20136851 |
| mean anomaly at epoch: | 101.1575° |
| orbit number at epoch: | 94631 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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