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 22334.73098965 -.00000454 00000-0 00000+0 0 9994
2 25544 51.6408 231.5387 0003844 110.3982 316.0051 15.49602948371014
| Epoch (UTC): | 30 November 2022 17:32:37 |
| Eccentricity: | 0.0003844 |
| inclination: | 51.6408° |
| perigee height: | 415 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 231.5387° |
| argument of perigee: | 110.3982° |
| revolutions per day: | 15.49602948 |
| mean anomaly at epoch: | 316.0051° |
| orbit number at epoch: | 37101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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