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 23154.12423077 .00000313 00000-0 11141-3 0 9995
2 17304 74.0600 48.6029 0028577 61.5652 298.8377 14.38047481905937
| Epoch (UTC): | 03 June 2023 02:58:53 |
| Eccentricity: | 0.0028577 |
| inclination: | 74.0600° |
| perigee height: | 744 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 48.6029° |
| argument of perigee: | 61.5652° |
| revolutions per day: | 14.38047481 |
| mean anomaly at epoch: | 298.8377° |
| orbit number at epoch: | 90593 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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