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 22889U 93070B 23153.50077850 -.00000020 00000-0 -34473-4 0 9993
2 22889 82.9434 138.3732 0048424 248.0779 111.5228 13.78028723487096
| Epoch (UTC): | 02 June 2023 12:01:07 |
| Eccentricity: | 0.0048424 |
| inclination: | 82.9434° |
| perigee height: | 935 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 138.3732° |
| argument of perigee: | 248.0779° |
| revolutions per day: | 13.78028723 |
| mean anomaly at epoch: | 111.5228° |
| orbit number at epoch: | 48709 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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