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 00059U 60013B 22228.68988234 .00000135 00000-0 65995-4 0 9995
2 00059 28.2478 118.8723 0189134 79.0036 283.1722 13.53003254 53344
| Epoch (UTC): | 16 August 2022 16:33:25 |
| Eccentricity: | 0.0189134 |
| inclination: | 28.2478° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 118.8723° |
| argument of perigee: | 79.0036° |
| revolutions per day: | 13.53003254 |
| mean anomaly at epoch: | 283.1722° |
| orbit number at epoch: | 5334 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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