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 23155.62384084 .00000171 00000-0 10783-3 0 9990
2 17974 71.0084 359.7973 0015628 301.7630 114.6905 14.17359455865093
| Epoch (UTC): | 04 June 2023 14:58:19 |
| Eccentricity: | 0.0015628 |
| inclination: | 71.0084° |
| perigee height: | 823 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 359.7973° |
| argument of perigee: | 301.7630° |
| revolutions per day: | 14.17359455 |
| mean anomaly at epoch: | 114.6905° |
| orbit number at epoch: | 86509 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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