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 18748U 88001A 23332.81728215 .00015248 00000-0 60189-3 0 9999
2 18748 82.4679 245.8870 0012034 19.8469 340.3235 15.25350531962677
| Epoch (UTC): | 28 November 2023 19:36:53 |
| Eccentricity: | 0.0012034 |
| inclination: | 82.4679° |
| perigee height: | 481 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 245.8870° |
| argument of perigee: | 19.8469° |
| revolutions per day: | 15.25350531 |
| mean anomaly at epoch: | 340.3235° |
| orbit number at epoch: | 96267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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