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 27597U 02056A 25117.48996280 .00000787 00000-0 32864-3 0 9993
2 27597 98.7346 69.7103 0001134 133.9656 226.1619 14.29008067165137
| Epoch (UTC): | 27 April 2025 11:45:32 |
| Eccentricity: | 0.0001134 |
| inclination: | 98.7346° |
| perigee height: | 794 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 69.7103° |
| argument of perigee: | 133.9656° |
| revolutions per day: | 14.29008067 |
| mean anomaly at epoch: | 226.1619° |
| orbit number at epoch: | 16513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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