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 23161.05314815 .00013937 00000-0 24614-3 0 9993
2 25544 51.6422 3.8974 0005491 67.8121 67.8666 15.50633390400689
| Epoch (UTC): | 10 June 2023 01:16:32 |
| Eccentricity: | 0.0005491 |
| inclination: | 51.6422° |
| perigee height: | 411 km |
| apogee height: | 418 km |
| right ascension of ascending node: | 3.8974° |
| argument of perigee: | 67.8121° |
| revolutions per day: | 15.50633390 |
| mean anomaly at epoch: | 67.8666° |
| orbit number at epoch: | 40068 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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