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 25136.93321701 .00013307 00000-0 80935-3 0 9994
2 31702 63.3198 8.1930 0509153 37.6071 325.9484 14.41706395 53433
| Epoch (UTC): | 16 May 2025 22:23:49 |
| Eccentricity: | 0.0509153 |
| inclination: | 63.3198° |
| perigee height: | 390 km |
| apogee height: | 1116 km |
| right ascension of ascending node: | 8.1930° |
| argument of perigee: | 37.6071° |
| revolutions per day: | 14.41706395 |
| mean anomaly at epoch: | 325.9484° |
| orbit number at epoch: | 5343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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