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 25544U 98067A 23266.57440972 .00017149 00000-0 31239-3 0 9990
2 25544 51.6416 201.1931 0005938 51.1971 290.7201 15.49566993417045
| Epoch (UTC): | 23 September 2023 13:47:09 |
| Eccentricity: | 0.0005938 |
| inclination: | 51.6416° |
| perigee height: | 414 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 201.1931° |
| argument of perigee: | 51.1971° |
| revolutions per day: | 15.49566993 |
| mean anomaly at epoch: | 290.7201° |
| orbit number at epoch: | 41704 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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