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 23081.88188931 .00002862 00000-0 28049-3 0 9993
2 43678 98.0051 224.2028 0010792 88.2351 272.0108 14.93050194239380
| Epoch (UTC): | 22 March 2023 21:09:55 |
| Eccentricity: | 0.0010792 |
| inclination: | 98.0051° |
| perigee height: | 581 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 224.2028° |
| argument of perigee: | 88.2351° |
| revolutions per day: | 14.93050194 |
| mean anomaly at epoch: | 272.0108° |
| orbit number at epoch: | 23938 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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