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 00012U 59001B 22228.77015864 .00000109 00000-0 43195-4 0 9998
2 00012 32.9122 105.1883 1666007 271.9802 69.1663 11.44691714370532
| Epoch (UTC): | 16 August 2022 18:29:01 |
| Eccentricity: | 0.1666007 |
| inclination: | 32.9122° |
| perigee height: | 553 km |
| apogee height: | 3324 km |
| right ascension of ascending node: | 105.1883° |
| argument of perigee: | 271.9802° |
| revolutions per day: | 11.44691714 |
| mean anomaly at epoch: | 69.1663° |
| orbit number at epoch: | 37053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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