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 22219U 92076A 24261.60144963 .00000262 00000-0 16279-3 0 9996
2 22219 71.0603 62.7951 0020550 299.3324 60.5745 14.13918277642315
| Epoch (UTC): | 17 September 2024 14:26:05 |
| Eccentricity: | 0.0020550 |
| inclination: | 71.0603° |
| perigee height: | 831 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 62.7951° |
| argument of perigee: | 299.3324° |
| revolutions per day: | 14.13918277 |
| mean anomaly at epoch: | 60.5745° |
| orbit number at epoch: | 64231 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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