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 40025U 14033R 19228.77120053 +.00000123 +00000-0 +19106-4 0 9996
2 40025 097.9036 148.3574 0011329 220.3785 139.6592 14.88965893279602
| Epoch (UTC): | 16 August 2019 18:30:31 |
| Eccentricity: | 0.0011329 |
| inclination: | 97.9036° |
| perigee height: | 593 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 148.3574° |
| argument of perigee: | 220.3785° |
| revolutions per day: | 14.88965893 |
| mean anomaly at epoch: | 139.6592° |
| orbit number at epoch: | 27960 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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