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 17974U 87041B 23159.49839942 .00000250 00000-0 14723-3 0 9993
2 17974 71.0084 351.6317 0015764 296.6541 83.8057 14.17361503865643
| Epoch (UTC): | 08 June 2023 11:57:41 |
| Eccentricity: | 0.0015764 |
| inclination: | 71.0084° |
| perigee height: | 823 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 351.6317° |
| argument of perigee: | 296.6541° |
| revolutions per day: | 14.17361503 |
| mean anomaly at epoch: | 83.8057° |
| orbit number at epoch: | 86564 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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