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 21667U 91059B 23154.59837013 .00000005 00000-0 -10524-4 0 9999
2 21667 82.9064 187.5939 0019533 306.6490 166.0977 13.75152378594673
| Epoch (UTC): | 03 June 2023 14:21:39 |
| Eccentricity: | 0.0019533 |
| inclination: | 82.9064° |
| perigee height: | 967 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 187.5939° |
| argument of perigee: | 306.6490° |
| revolutions per day: | 13.75152378 |
| mean anomaly at epoch: | 166.0977° |
| orbit number at epoch: | 59467 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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