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 43737U 18096U 22279.81645878 .00033210 00000-0 76244-3 0 9992
2 43737 97.3498 5.2383 0016163 10.2170 349.9403 15.42501073215430
| Epoch (UTC): | 06 October 2022 19:35:42 |
| Eccentricity: | 0.0016163 |
| inclination: | 97.3498° |
| perigee height: | 428 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 5.2383° |
| argument of perigee: | 10.2170° |
| revolutions per day: | 15.42501073 |
| mean anomaly at epoch: | 349.9403° |
| orbit number at epoch: | 21543 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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