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 23080.83902292 .00015283 00000-0 28135-3 0 9999
2 25544 51.6417 41.2842 0006128 116.9281 332.0201 15.49359891388242
| Epoch (UTC): | 21 March 2023 20:08:11 |
| Eccentricity: | 0.0006128 |
| inclination: | 51.6417° |
| perigee height: | 414 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 41.2842° |
| argument of perigee: | 116.9281° |
| revolutions per day: | 15.49359891 |
| mean anomaly at epoch: | 332.0201° |
| orbit number at epoch: | 38824 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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