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 23338.91528137 .00000166 00000-0 10469-3 0 9995
2 00059 28.2459 197.5590 0189052 108.0090 254.1152 13.53050475117759
| Epoch (UTC): | 04 December 2023 21:58:00 |
| Eccentricity: | 0.0189052 |
| inclination: | 28.2459° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 197.5590° |
| argument of perigee: | 108.0090° |
| revolutions per day: | 13.53050475 |
| mean anomaly at epoch: | 254.1152° |
| orbit number at epoch: | 11775 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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