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 23341.45332294 .00000382 00000-0 17146-3 0 9993
2 27597 98.6696 284.2134 0000440 128.2045 231.9176 14.28115073 92743
| Epoch (UTC): | 07 December 2023 10:52:47 |
| Eccentricity: | 0.0000440 |
| inclination: | 98.6696° |
| perigee height: | 798 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 284.2134° |
| argument of perigee: | 128.2045° |
| revolutions per day: | 14.28115073 |
| mean anomaly at epoch: | 231.9176° |
| orbit number at epoch: | 9274 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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