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 16369U 85116B 24348.78520749 .00000072 00000-0 56782-4 0 9990
2 16369 82.9365 112.8739 0037253 61.4960 105.0219 13.77088137958563
| Epoch (UTC): | 13 December 2024 18:50:41 |
| Eccentricity: | 0.0037253 |
| inclination: | 82.9365° |
| perigee height: | 947 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 112.8739° |
| argument of perigee: | 61.4960° |
| revolutions per day: | 13.77088137 |
| mean anomaly at epoch: | 105.0219° |
| orbit number at epoch: | 95856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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