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 40042U 14033AJ 19345.73015250 +.00000298 +00000-0 +37833-4 0 9993
2 40042 097.9177 265.5417 0014226 185.4649 174.6415 14.88758605296911
| Epoch (UTC): | 11 December 2019 17:31:25 |
| Eccentricity: | 0.0014226 |
| inclination: | 97.9177° |
| perigee height: | 592 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 265.5417° |
| argument of perigee: | 185.4649° |
| revolutions per day: | 14.88758605 |
| mean anomaly at epoch: | 174.6415° |
| orbit number at epoch: | 29691 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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