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 32954U 08025B 19016.67719047 .00000001 00000-0 -68301-4 0 9990
2 32954 82.4999 241.0494 0020984 114.4402 245.8856 12.42698402483178
| Epoch (UTC): | 16 January 2019 16:15:09 |
| Eccentricity: | 0.0020984 |
| inclination: | 82.4999° |
| perigee height: | 1478 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 241.0494° |
| argument of perigee: | 114.4402° |
| revolutions per day: | 12.42698402 |
| mean anomaly at epoch: | 245.8856° |
| orbit number at epoch: | 48317 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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