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 14506U 83113A 22141.50083736 .00000310 00000-0 14057-3 0 9998
2 14506 98.2875 330.6286 0010267 311.2986 102.5571 14.28250089 3026
| Epoch (UTC): | 21 May 2022 12:01:12 |
| Eccentricity: | 0.0010267 |
| inclination: | 98.2875° |
| perigee height: | 790 km |
| apogee height: | 805 km |
| right ascension of ascending node: | 330.6286° |
| argument of perigee: | 311.2986° |
| revolutions per day: | 14.28250089 |
| mean anomaly at epoch: | 102.5571° |
| orbit number at epoch: | 302 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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