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 22181.25741613 .00000513 00000-0 56107-4 0 9994
2 43678 97.9721 314.6736 0008582 239.1480 120.8914 14.92188228199767
| Epoch (UTC): | 30 June 2022 06:10:40 |
| Eccentricity: | 0.0008582 |
| inclination: | 97.9721° |
| perigee height: | 585 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 314.6736° |
| argument of perigee: | 239.1480° |
| revolutions per day: | 14.92188228 |
| mean anomaly at epoch: | 120.8914° |
| orbit number at epoch: | 19976 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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