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 23815U 96014B 23033.36710169 .00000192 00000-0 77298-4 0 9992
2 23815 90.0375 336.9723 0020772 206.2605 153.7537 14.24945082398333
| Epoch (UTC): | 02 February 2023 08:48:37 |
| Eccentricity: | 0.0020772 |
| inclination: | 90.0375° |
| perigee height: | 794 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 336.9723° |
| argument of perigee: | 206.2605° |
| revolutions per day: | 14.24945082 |
| mean anomaly at epoch: | 153.7537° |
| orbit number at epoch: | 39833 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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