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 24278U 96046B 22222.48593817 .00000022 00000-0 55728-4 0 9998
2 24278 98.5154 238.7434 0351002 142.9689 219.6238 13.53118446283165
| Epoch (UTC): | 10 August 2022 11:39:45 |
| Eccentricity: | 0.0351002 |
| inclination: | 98.5154° |
| perigee height: | 800 km |
| apogee height: | 1322 km |
| right ascension of ascending node: | 238.7434° |
| argument of perigee: | 142.9689° |
| revolutions per day: | 13.53118446 |
| mean anomaly at epoch: | 219.6238° |
| orbit number at epoch: | 28316 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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