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 23275.87908750 .00020961 00000-0 37800-3 0 9992
2 25544 51.6412 155.1166 0005263 66.9479 19.1881 15.49709683418499
| Epoch (UTC): | 02 October 2023 21:05:53 |
| Eccentricity: | 0.0005263 |
| inclination: | 51.6412° |
| perigee height: | 414 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 155.1166° |
| argument of perigee: | 66.9479° |
| revolutions per day: | 15.49709683 |
| mean anomaly at epoch: | 19.1881° |
| orbit number at epoch: | 41849 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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