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 23337.44829795 .00000107 00000-0 14012-3 0 9996
2 00116 66.8106 357.8953 0078568 207.4771 152.2145 13.91974537167709
| Epoch (UTC): | 03 December 2023 10:45:32 |
| Eccentricity: | 0.0078568 |
| inclination: | 66.8106° |
| perigee height: | 864 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 357.8953° |
| argument of perigee: | 207.4771° |
| revolutions per day: | 13.91974537 |
| mean anomaly at epoch: | 152.2145° |
| orbit number at epoch: | 16770 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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