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 22177.83750927 .00000373 00000-0 42426-4 0 9994
2 43678 97.9717 311.2129 0008490 252.6109 107.4181 14.92183905199255
| Epoch (UTC): | 26 June 2022 20:06:00 |
| Eccentricity: | 0.0008490 |
| inclination: | 97.9717° |
| perigee height: | 585 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 311.2129° |
| argument of perigee: | 252.6109° |
| revolutions per day: | 14.92183905 |
| mean anomaly at epoch: | 107.4181° |
| orbit number at epoch: | 19925 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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