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 22226.67949722 .00005748 00000-0 10796-3 0 9990
2 25544 51.6423 46.8191 0005608 120.4183 342.1125 15.50176693354250
| Epoch (UTC): | 14 August 2022 16:18:28 |
| Eccentricity: | 0.0005608 |
| inclination: | 51.6423° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 46.8191° |
| argument of perigee: | 120.4183° |
| revolutions per day: | 15.50176693 |
| mean anomaly at epoch: | 342.1125° |
| orbit number at epoch: | 35425 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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