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 00116U 61015A 22274.55814157 -.00000006 00000-0 54032-4 0 9999
2 00116 66.8106 324.1624 0072032 147.4827 213.0720 13.91847299108159
| Epoch (UTC): | 01 October 2022 13:23:43 |
| Eccentricity: | 0.0072032 |
| inclination: | 66.8106° |
| perigee height: | 869 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 324.1624° |
| argument of perigee: | 147.4827° |
| revolutions per day: | 13.91847299 |
| mean anomaly at epoch: | 213.0720° |
| orbit number at epoch: | 10815 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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