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 16327U 85113B 22147.69629424 .00000353 00000-0 39715-4 0 9995
2 16327 82.5354 204.2864 0019806 149.6465 332.8780 14.83634829948407
| Epoch (UTC): | 27 May 2022 16:42:39 |
| Eccentricity: | 0.0019806 |
| inclination: | 82.5354° |
| perigee height: | 604 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 204.2864° |
| argument of perigee: | 149.6465° |
| revolutions per day: | 14.83634829 |
| mean anomaly at epoch: | 332.8780° |
| orbit number at epoch: | 94840 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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