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 31702U 07027B 25134.01993138 .00013914 00000-0 84783-3 0 9999
2 31702 63.3205 17.0558 0509186 37.5590 325.9929 14.41622656 53013
| Epoch (UTC): | 14 May 2025 00:28:42 |
| Eccentricity: | 0.0509186 |
| inclination: | 63.3205° |
| perigee height: | 390 km |
| apogee height: | 1116 km |
| right ascension of ascending node: | 17.0558° |
| argument of perigee: | 37.5590° |
| revolutions per day: | 14.41622656 |
| mean anomaly at epoch: | 325.9929° |
| orbit number at epoch: | 5301 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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