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 18821U 88005B 23149.71375497 .00000044 00000-0 26151-4 0 9990
2 18821 82.5404 132.8061 0014161 352.6715 7.4236 13.85148850785744
| Epoch (UTC): | 29 May 2023 17:07:48 |
| Eccentricity: | 0.0014161 |
| inclination: | 82.5404° |
| perigee height: | 935 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 132.8061° |
| argument of perigee: | 352.6715° |
| revolutions per day: | 13.85148850 |
| mean anomaly at epoch: | 7.4236° |
| orbit number at epoch: | 78574 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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