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 40015U 14033F 23155.56444251 .00000888 00000-0 12347-3 0 9992
2 40015 97.6090 356.3780 0037169 35.8000 324.5693 14.79681963483367
| Epoch (UTC): | 04 June 2023 13:32:47 |
| Eccentricity: | 0.0037169 |
| inclination: | 97.6090° |
| perigee height: | 604 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 356.3780° |
| argument of perigee: | 35.8000° |
| revolutions per day: | 14.79681963 |
| mean anomaly at epoch: | 324.5693° |
| orbit number at epoch: | 48336 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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