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 22826U 93061D 23155.90254314 .00000147 00000-0 73679-4 0 9991
2 22826 98.8361 198.4580 0010134 90.3510 269.8833 14.30665765548806
| Epoch (UTC): | 04 June 2023 21:39:39 |
| Eccentricity: | 0.0010134 |
| inclination: | 98.8361° |
| perigee height: | 782 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 198.4580° |
| argument of perigee: | 90.3510° |
| revolutions per day: | 14.30665765 |
| mean anomaly at epoch: | 269.8833° |
| orbit number at epoch: | 54880 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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