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 31701U 07027A 25098.82360922 0.00000200 00000-0 21206-3 0 03
2 31701 63.3825 358.2043 0425183 22.5216 337.4784 13.40970841 00
| Epoch (UTC): | 08 April 2025 19:45:59 |
| Eccentricity: | 0.0425183 |
| inclination: | 63.3825° |
| perigee height: | 787 km |
| apogee height: | 1424 km |
| right ascension of ascending node: | 358.2043° |
| argument of perigee: | 22.5216° |
| revolutions per day: | 13.40970841 |
| mean anomaly at epoch: | 337.4784° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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