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 22334.27113061 -.00000013 00000-0 48833-4 0 9991
2 00116 66.8080 178.1704 0069221 102.1866 258.6978 13.91859753116464
| Epoch (UTC): | 30 November 2022 06:30:25 |
| Eccentricity: | 0.0069221 |
| inclination: | 66.8080° |
| perigee height: | 871 km |
| apogee height: | 972 km |
| right ascension of ascending node: | 178.1704° |
| argument of perigee: | 102.1866° |
| revolutions per day: | 13.91859753 |
| mean anomaly at epoch: | 258.6978° |
| orbit number at epoch: | 11646 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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