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 22627U 93024B 24283.85336438 .00001526 00000-0 20112-3 0 9999
2 22627 82.5207 138.1525 0021683 229.9726 129.9585 14.79369299696871
| Epoch (UTC): | 09 October 2024 20:28:50 |
| Eccentricity: | 0.0021683 |
| inclination: | 82.5207° |
| perigee height: | 616 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 138.1525° |
| argument of perigee: | 229.9726° |
| revolutions per day: | 14.79369299 |
| mean anomaly at epoch: | 129.9585° |
| orbit number at epoch: | 69687 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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