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 23334.88360323 .00024407 00000-0 43434-3 0 9996
2 25544 51.6428 222.8885 0000854 1.5392 103.8408 15.49998542427643
| Epoch (UTC): | 30 November 2023 21:12:23 |
| Eccentricity: | 0.0000854 |
| inclination: | 51.6428° |
| perigee height: | 416 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 222.8885° |
| argument of perigee: | 1.5392° |
| revolutions per day: | 15.49998542 |
| mean anomaly at epoch: | 103.8408° |
| orbit number at epoch: | 42764 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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