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 23342U 94074A 19345.72028425 .00000050 00000-0 13587-4 0 9993
2 23342 97.9587 31.8133 0001895 81.1147 279.0279 14.79412380351953
| Epoch (UTC): | 11 December 2019 17:17:12 |
| Eccentricity: | 0.0001895 |
| inclination: | 97.9587° |
| perigee height: | 630 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 31.8133° |
| argument of perigee: | 81.1147° |
| revolutions per day: | 14.79412380 |
| mean anomaly at epoch: | 279.0279° |
| orbit number at epoch: | 35195 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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