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 22148.51988808 .00000019 00000-0 73543-4 0 9991
2 00116 66.8100 272.3079 0081262 234.3855 124.9636 13.91830203 90617
| Epoch (UTC): | 28 May 2022 12:28:38 |
| Eccentricity: | 0.0081262 |
| inclination: | 66.8100° |
| perigee height: | 863 km |
| apogee height: | 981 km |
| right ascension of ascending node: | 272.3079° |
| argument of perigee: | 234.3855° |
| revolutions per day: | 13.91830203 |
| mean anomaly at epoch: | 124.9636° |
| orbit number at epoch: | 9061 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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