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 23265.94708924 .00017650 00000-0 32149-3 0 9992
2 25544 51.6420 204.2958 0005837 49.6219 30.5458 15.49546865416957
| Epoch (UTC): | 22 September 2023 22:43:48 |
| Eccentricity: | 0.0005837 |
| inclination: | 51.6420° |
| perigee height: | 414 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 204.2958° |
| argument of perigee: | 49.6219° |
| revolutions per day: | 15.49546865 |
| mean anomaly at epoch: | 30.5458° |
| orbit number at epoch: | 41695 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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