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 00046U 60007B 22220.94195710 .00000193 00000-0 59871-4 0 9994
2 00046 66.6898 91.6995 0216705 267.7655 89.8627 14.49749121252510
| Epoch (UTC): | 08 August 2022 22:36:25 |
| Eccentricity: | 0.0216705 |
| inclination: | 66.6898° |
| perigee height: | 572 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 91.6995° |
| argument of perigee: | 267.7655° |
| revolutions per day: | 14.49749121 |
| mean anomaly at epoch: | 89.8627° |
| orbit number at epoch: | 25251 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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