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 23081.03898101 .00015358 00000-0 28263-3 0 9990
2 25544 51.6417 40.2943 0006096 117.6201 7.3764 15.49366819388274
| Epoch (UTC): | 22 March 2023 00:56:07 |
| Eccentricity: | 0.0006096 |
| inclination: | 51.6417° |
| perigee height: | 414 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 40.2943° |
| argument of perigee: | 117.6201° |
| revolutions per day: | 15.49366819 |
| mean anomaly at epoch: | 7.3764° |
| orbit number at epoch: | 38827 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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