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 36089U 09061B 23339.52118341 .00000979 00000-0 25116-3 0 9990
2 36089 98.3335 301.9185 0080165 352.6895 7.3124 14.50666375743930
| Epoch (UTC): | 05 December 2023 12:30:30 |
| Eccentricity: | 0.0080165 |
| inclination: | 98.3335° |
| perigee height: | 666 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 301.9185° |
| argument of perigee: | 352.6895° |
| revolutions per day: | 14.50666375 |
| mean anomaly at epoch: | 7.3124° |
| orbit number at epoch: | 74393 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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