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 43678U 18084H 25138.88384537 .00002767 00000-0 23823-3 0 9997
2 43678 98.1018 314.1827 0007812 6.1889 353.9427 14.98232100357135
| Epoch (UTC): | 18 May 2025 21:12:44 |
| Eccentricity: | 0.0007812 |
| inclination: | 98.1018° |
| perigee height: | 567 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 314.1827° |
| argument of perigee: | 6.1889° |
| revolutions per day: | 14.98232100 |
| mean anomaly at epoch: | 353.9427° |
| orbit number at epoch: | 35713 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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