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 19119U 88039A 23336.58798223 .00000047 00000-0 48502-4 0 9994
2 19119 71.0017 186.3285 0009382 64.1121 3.0989 14.15369634835624
| Epoch (UTC): | 02 December 2023 14:06:41 |
| Eccentricity: | 0.0009382 |
| inclination: | 71.0017° |
| perigee height: | 834 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 186.3285° |
| argument of perigee: | 64.1121° |
| revolutions per day: | 14.15369634 |
| mean anomaly at epoch: | 3.0989° |
| orbit number at epoch: | 83562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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