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 22027.47837506 .00000681 00000-0 38396-3 0 9998
2 00012 32.9115 89.8935 1666013 293.1012 50.2789 11.44510879347464
| Epoch (UTC): | 27 January 2022 11:28:51 |
| Eccentricity: | 0.1666013 |
| inclination: | 32.9115° |
| perigee height: | 553 km |
| apogee height: | 3325 km |
| right ascension of ascending node: | 89.8935° |
| argument of perigee: | 293.1012° |
| revolutions per day: | 11.44510879 |
| mean anomaly at epoch: | 50.2789° |
| orbit number at epoch: | 34746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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