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 00059U 60013B 23027.26463803 .00000165 00000-0 10614-3 0 9997
2 00059 28.2505 358.5869 0189099 12.0064 348.4910 13.53016270 75516
| Epoch (UTC): | 27 January 2023 06:21:04 |
| Eccentricity: | 0.0189099 |
| inclination: | 28.2505° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 358.5869° |
| argument of perigee: | 12.0064° |
| revolutions per day: | 13.53016270 |
| mean anomaly at epoch: | 348.4910° |
| orbit number at epoch: | 7551 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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