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 17296U 87003B 23154.47363174 .00000478 00000-0 54621-4 0 9994
2 17296 82.5278 148.2045 0017293 239.2677 120.6836 14.83847865944794
| Epoch (UTC): | 03 June 2023 11:22:01 |
| Eccentricity: | 0.0017293 |
| inclination: | 82.5278° |
| perigee height: | 605 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 148.2045° |
| argument of perigee: | 239.2677° |
| revolutions per day: | 14.83847865 |
| mean anomaly at epoch: | 120.6836° |
| orbit number at epoch: | 94479 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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