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 23465U 95002C 19341.54458039 .00000038 00000-0 26017-4 0 9993
2 23465 82.9260 343.6608 0036287 301.9305 172.1300 13.71891806245263
| Epoch (UTC): | 07 December 2019 13:04:11 |
| Eccentricity: | 0.0036287 |
| inclination: | 82.9260° |
| perigee height: | 966 km |
| apogee height: | 1019 km |
| right ascension of ascending node: | 343.6608° |
| argument of perigee: | 301.9305° |
| revolutions per day: | 13.71891806 |
| mean anomaly at epoch: | 172.1300° |
| orbit number at epoch: | 24526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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