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 19082.78497996 .00000307 00000-0 39050-4 0 9991
2 40042 97.9144 2.8733 0014305 340.9506 19.1174 14.88596707258305
| Epoch (UTC): | 23 March 2019 18:50:22 |
| Eccentricity: | 0.0014305 |
| inclination: | 97.9144° |
| perigee height: | 592 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 2.8733° |
| argument of perigee: | 340.9506° |
| revolutions per day: | 14.88596707 |
| mean anomaly at epoch: | 19.1174° |
| orbit number at epoch: | 25830 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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