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 23029.41460570 .00000026 00000-0 79151-4 0 9999
2 00116 66.8103 31.1228 0070059 55.8201 304.9493 13.91873658124834
| Epoch (UTC): | 29 January 2023 09:57:01 |
| Eccentricity: | 0.0070059 |
| inclination: | 66.8103° |
| perigee height: | 871 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 31.1228° |
| argument of perigee: | 55.8201° |
| revolutions per day: | 13.91873658 |
| mean anomaly at epoch: | 304.9493° |
| orbit number at epoch: | 12483 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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