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 39440U 13066AA 22179.43041992 .00000994 00000-0 14072-3 0 9998
2 39440 97.7266 136.5258 0080333 95.6875 265.3502 14.77030748461900
| Epoch (UTC): | 28 June 2022 10:19:48 |
| Eccentricity: | 0.0080333 |
| inclination: | 97.7266° |
| perigee height: | 582 km |
| apogee height: | 695 km |
| right ascension of ascending node: | 136.5258° |
| argument of perigee: | 95.6875° |
| revolutions per day: | 14.77030748 |
| mean anomaly at epoch: | 265.3502° |
| orbit number at epoch: | 46190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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