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 22146.28913208 .00010641 00000-0 19625-3 0 9996
2 25544 51.6432 85.0432 0005079 158.8310 1.4584 15.49689966341780
| Epoch (UTC): | 26 May 2022 06:56:21 |
| Eccentricity: | 0.0005079 |
| inclination: | 51.6432° |
| perigee height: | 414 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 85.0432° |
| argument of perigee: | 158.8310° |
| revolutions per day: | 15.49689966 |
| mean anomaly at epoch: | 1.4584° |
| orbit number at epoch: | 34178 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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