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 24278.86828709 .00002090 00000-0 85049-3 0 9994
2 27597 98.7022 225.1662 0002215 80.9934 279.1497 14.28587293135914
| Epoch (UTC): | 04 October 2024 20:50:20 |
| Eccentricity: | 0.0002215 |
| inclination: | 98.7022° |
| perigee height: | 795 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 225.1662° |
| argument of perigee: | 80.9934° |
| revolutions per day: | 14.28587293 |
| mean anomaly at epoch: | 279.1497° |
| orbit number at epoch: | 13591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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