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 43440U 18040B 22179.09247398 .00005233 00000-0 23354-3 0 9994
2 43440 97.2444 237.7635 0012354 19.0978 69.8132 15.21730584231336
| Epoch (UTC): | 28 June 2022 02:13:09 |
| Eccentricity: | 0.0012354 |
| inclination: | 97.2444° |
| perigee height: | 492 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 237.7635° |
| argument of perigee: | 19.0978° |
| revolutions per day: | 15.21730584 |
| mean anomaly at epoch: | 69.8132° |
| orbit number at epoch: | 23133 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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