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 43116U 18004F 23088.73155970 .00058418 00000-0 12899-2 0 9993
2 43116 97.3416 169.1502 0005566 62.5144 297.6669 15.43658733290084
| Epoch (UTC): | 29 March 2023 17:33:26 |
| Eccentricity: | 0.0005566 |
| inclination: | 97.3416° |
| perigee height: | 431 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 169.1502° |
| argument of perigee: | 62.5144° |
| revolutions per day: | 15.43658733 |
| mean anomaly at epoch: | 297.6669° |
| orbit number at epoch: | 29008 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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