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 23155.82552891 .00012207 00000-0 21782-3 0 9991
2 25544 51.6423 29.8185 0005525 52.4285 43.3600 15.50474395399874
| Epoch (UTC): | 04 June 2023 19:48:45 |
| Eccentricity: | 0.0005525 |
| inclination: | 51.6423° |
| perigee height: | 411 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 29.8185° |
| argument of perigee: | 52.4285° |
| revolutions per day: | 15.50474395 |
| mean anomaly at epoch: | 43.3600° |
| orbit number at epoch: | 39987 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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