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 27598U 02056B 23342.45379705 .00000142 00000-0 73571-4 0 9992
2 27598 98.7306 291.2516 0009687 141.8003 218.3866 14.29069320 94079
| Epoch (UTC): | 08 December 2023 10:53:28 |
| Eccentricity: | 0.0009687 |
| inclination: | 98.7306° |
| perigee height: | 788 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 291.2516° |
| argument of perigee: | 141.8003° |
| revolutions per day: | 14.29069320 |
| mean anomaly at epoch: | 218.3866° |
| orbit number at epoch: | 9407 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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