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 23036.31273719 .00000058 00000-0 10317-3 0 9996
2 00116 66.8112 14.2570 0070429 50.6031 310.1256 13.91875497125796
| Epoch (UTC): | 05 February 2023 07:30:20 |
| Eccentricity: | 0.0070429 |
| inclination: | 66.8112° |
| perigee height: | 870 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 14.2570° |
| argument of perigee: | 50.6031° |
| revolutions per day: | 13.91875497 |
| mean anomaly at epoch: | 310.1256° |
| orbit number at epoch: | 12579 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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