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 22220.91851154 .00000120 00000-0 48665-4 0 9996
2 00012 32.9082 132.6711 1665603 230.6923 113.3947 11.44690518369636
| Epoch (UTC): | 08 August 2022 22:02:39 |
| Eccentricity: | 0.1665603 |
| inclination: | 32.9082° |
| perigee height: | 553 km |
| apogee height: | 3323 km |
| right ascension of ascending node: | 132.6711° |
| argument of perigee: | 230.6923° |
| revolutions per day: | 11.44690518 |
| mean anomaly at epoch: | 113.3947° |
| orbit number at epoch: | 36963 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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