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 23161.14837963 +.00002451 00000-0 +94548-4 0 08
2 43477 88.9877 350.1178 0016441 70.1872 6.9857 15.26125416280930
| Epoch (UTC): | 10 June 2023 03:33:40 |
| Eccentricity: | 0.0016441 |
| inclination: | 88.9877° |
| perigee height: | 476 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 350.1178° |
| argument of perigee: | 70.1872° |
| revolutions per day: | 15.26125416 |
| mean anomaly at epoch: | 6.9857° |
| orbit number at epoch: | 28093 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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