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 23332.12744535 .00000206 00000-0 16007-3 0 9993
2 00059 28.2471 232.4328 0189001 51.0130 310.7089 13.53049152116833
| Epoch (UTC): | 28 November 2023 03:03:31 |
| Eccentricity: | 0.0189001 |
| inclination: | 28.2471° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 232.4328° |
| argument of perigee: | 51.0130° |
| revolutions per day: | 13.53049152 |
| mean anomaly at epoch: | 310.7089° |
| orbit number at epoch: | 11683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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