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 24283.84103292 .00001666 00000-0 68152-3 0 9995
2 27597 98.7030 230.1265 0002260 75.4808 284.6624 14.28602952136629
| Epoch (UTC): | 09 October 2024 20:11:05 |
| Eccentricity: | 0.0002260 |
| inclination: | 98.7030° |
| perigee height: | 795 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 230.1265° |
| argument of perigee: | 75.4808° |
| revolutions per day: | 14.28602952 |
| mean anomaly at epoch: | 284.6624° |
| orbit number at epoch: | 13662 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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