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 19922U 89028B 24278.99450937 .00000506 00000-0 49260-3 0 9994
2 19922 82.9558 248.2461 0035863 337.4635 22.4945 13.77391355784307
| Epoch (UTC): | 04 October 2024 23:52:05 |
| Eccentricity: | 0.0035863 |
| inclination: | 82.9558° |
| perigee height: | 947 km |
| apogee height: | 999 km |
| right ascension of ascending node: | 248.2461° |
| argument of perigee: | 337.4635° |
| revolutions per day: | 13.77391355 |
| mean anomaly at epoch: | 22.4945° |
| orbit number at epoch: | 78430 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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