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 43476U 18047A 23150.66018501 +.00002124 00000-0 +82064-4 0 08
2 43476 88.9876 351.5431 0016978 103.5451 353.9070 15.26064791279336
| Epoch (UTC): | 30 May 2023 15:50:39 |
| Eccentricity: | 0.0016978 |
| inclination: | 88.9876° |
| perigee height: | 476 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 351.5431° |
| argument of perigee: | 103.5451° |
| revolutions per day: | 15.26064791 |
| mean anomaly at epoch: | 353.9070° |
| orbit number at epoch: | 27933 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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