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 23264.54105509 .00017543 00000-0 32015-3 0 9990
2 25544 51.6422 211.2563 0005854 43.1951 108.5454 15.49496080416731
| Epoch (UTC): | 21 September 2023 12:59:07 |
| Eccentricity: | 0.0005854 |
| inclination: | 51.6422° |
| perigee height: | 414 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 211.2563° |
| argument of perigee: | 43.1951° |
| revolutions per day: | 15.49496080 |
| mean anomaly at epoch: | 108.5454° |
| orbit number at epoch: | 41673 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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