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 23027.47450459 .00000031 00000-0 83116-4 0 9990
2 00116 66.8101 35.8667 0069959 57.3012 303.4788 13.91873227124567
| Epoch (UTC): | 27 January 2023 11:23:17 |
| Eccentricity: | 0.0069959 |
| inclination: | 66.8101° |
| perigee height: | 871 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 35.8667° |
| argument of perigee: | 57.3012° |
| revolutions per day: | 13.91873227 |
| mean anomaly at epoch: | 303.4788° |
| orbit number at epoch: | 12456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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