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 23027.86419706 .00008871 00000-0 41949-3 0 9994
2 18748 82.4693 191.3497 0012700 357.0079 3.1077 15.19176773916020
| Epoch (UTC): | 27 January 2023 20:44:26 |
| Eccentricity: | 0.0012700 |
| inclination: | 82.4693° |
| perigee height: | 499 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 191.3497° |
| argument of perigee: | 357.0079° |
| revolutions per day: | 15.19176773 |
| mean anomaly at epoch: | 3.1077° |
| orbit number at epoch: | 91602 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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