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 23093U 94024B 23150.12756416 .00000030 00000-0 14590-4 0 9995
2 23093 82.9443 297.9502 0010911 40.0427 320.1533 13.77976462930654
| Epoch (UTC): | 30 May 2023 03:03:41 |
| Eccentricity: | 0.0010911 |
| inclination: | 82.9443° |
| perigee height: | 963 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 297.9502° |
| argument of perigee: | 40.0427° |
| revolutions per day: | 13.77976462 |
| mean anomaly at epoch: | 320.1533° |
| orbit number at epoch: | 93065 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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