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 23092.19857081 .00023445 00000-0 42617-3 0 9996
2 25544 51.6427 345.0502 0007074 144.3638 353.1809 15.49398123390009
| Epoch (UTC): | 02 April 2023 04:45:56 |
| Eccentricity: | 0.0007074 |
| inclination: | 51.6427° |
| perigee height: | 413 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 345.0502° |
| argument of perigee: | 144.3638° |
| revolutions per day: | 15.49398123 |
| mean anomaly at epoch: | 353.1809° |
| orbit number at epoch: | 39000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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