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 22229.97407703 .00005568 00000-0 10468-3 0 9990
2 25544 51.6431 30.4906 0005480 132.8897 7.8677 15.50215749354768
| Epoch (UTC): | 17 August 2022 23:22:40 |
| Eccentricity: | 0.0005480 |
| inclination: | 51.6431° |
| perigee height: | 412 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 30.4906° |
| argument of perigee: | 132.8897° |
| revolutions per day: | 15.50215749 |
| mean anomaly at epoch: | 7.8677° |
| orbit number at epoch: | 35476 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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