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 16624U 86014E 23088.28720234 .00010007 00000-0 83003-3 0 9992
2 16624 63.2990 46.7409 0910018 94.4233 276.1188 13.52415915188662
| Epoch (UTC): | 29 March 2023 06:53:34 |
| Eccentricity: | 0.0910018 |
| inclination: | 63.2990° |
| perigee height: | 386 km |
| apogee height: | 1740 km |
| right ascension of ascending node: | 46.7409° |
| argument of perigee: | 94.4233° |
| revolutions per day: | 13.52415915 |
| mean anomaly at epoch: | 276.1188° |
| orbit number at epoch: | 18866 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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