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 43477U 18047B 23029.63481479 +.00003325 00000-0 +13288-3 0 04
2 43477 88.9910 7.8921 0013586 195.1937 243.3260 15.24989002260881
| Epoch (UTC): | 29 January 2023 15:14:07 |
| Eccentricity: | 0.0013586 |
| inclination: | 88.9910° |
| perigee height: | 481 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 7.8921° |
| argument of perigee: | 195.1937° |
| revolutions per day: | 15.24989002 |
| mean anomaly at epoch: | 243.3260° |
| orbit number at epoch: | 26088 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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