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 16116U 85092B 23081.51448781 -.00000020 00000-0 00000+0 0 9993
2 16116 14.8906 356.3023 0004104 111.6838 98.1697 0.99326510 14150
| Epoch (UTC): | 22 March 2023 12:20:51 |
| Eccentricity: | 0.0004104 |
| inclination: | 14.8906° |
| perigee height: | 36036 km |
| apogee height: | 36071 km |
| right ascension of ascending node: | 356.3023° |
| argument of perigee: | 111.6838° |
| revolutions per day: | 0.99326510 |
| mean anomaly at epoch: | 98.1697° |
| orbit number at epoch: | 1415 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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