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 22208U 92073B 24281.85308003 .00000251 00000-0 24482-3 0 9990
2 22208 82.9222 197.7847 0034790 149.8361 271.9826 13.75326254602976
| Epoch (UTC): | 07 October 2024 20:28:26 |
| Eccentricity: | 0.0034790 |
| inclination: | 82.9222° |
| perigee height: | 955 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 197.7847° |
| argument of perigee: | 149.8361° |
| revolutions per day: | 13.75326254 |
| mean anomaly at epoch: | 271.9826° |
| orbit number at epoch: | 60297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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