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 17304U 87006B 23151.20242551 .00000261 00000-0 94326-4 0 9996
2 17304 74.0601 53.9769 0028502 67.8350 292.5824 14.38045366905512
| Epoch (UTC): | 31 May 2023 04:51:29 |
| Eccentricity: | 0.0028502 |
| inclination: | 74.0601° |
| perigee height: | 744 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 53.9769° |
| argument of perigee: | 67.8350° |
| revolutions per day: | 14.38045366 |
| mean anomaly at epoch: | 292.5824° |
| orbit number at epoch: | 90551 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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