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 9023U 76069B 23151.74539875 .00000276 00000-0 95781-4 0 9991
2 9023 74.0446 42.6273 0016784 28.1605 332.0454 14.40020586457763
| Epoch (UTC): | 31 May 2023 17:53:22 |
| Eccentricity: | 0.0016784 |
| inclination: | 74.0446° |
| perigee height: | 746 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 42.6273° |
| argument of perigee: | 28.1605° |
| revolutions per day: | 14.40020586 |
| mean anomaly at epoch: | 332.0454° |
| orbit number at epoch: | 45776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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