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 23335.71264821 .00019172 00000-0 34279-3 0 9995
2 25544 51.6422 218.7838 0001042 9.8014 44.7278 15.50025017427773
| Epoch (UTC): | 01 December 2023 17:06:12 |
| Eccentricity: | 0.0001042 |
| inclination: | 51.6422° |
| perigee height: | 416 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 218.7838° |
| argument of perigee: | 9.8014° |
| revolutions per day: | 15.50025017 |
| mean anomaly at epoch: | 44.7278° |
| orbit number at epoch: | 42777 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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