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 22268.70683716 .00009230 00000-0 16787-3 0 9994
2 25544 51.6424 198.5735 0002345 291.2893 138.5991 15.50278395360774
| Epoch (UTC): | 25 September 2022 16:57:50 |
| Eccentricity: | 0.0002345 |
| inclination: | 51.6424° |
| perigee height: | 414 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 198.5735° |
| argument of perigee: | 291.2893° |
| revolutions per day: | 15.50278395 |
| mean anomaly at epoch: | 138.5991° |
| orbit number at epoch: | 36077 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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