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 37792U 11044E 23339.28402688 .00001349 00000-0 19379-3 0 9995
2 37792 98.2571 233.6307 0057684 93.4363 267.3447 14.77088764662058
| Epoch (UTC): | 05 December 2023 06:48:59 |
| Eccentricity: | 0.0057684 |
| inclination: | 98.2571° |
| perigee height: | 598 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 233.6307° |
| argument of perigee: | 93.4363° |
| revolutions per day: | 14.77088764 |
| mean anomaly at epoch: | 267.3447° |
| orbit number at epoch: | 66205 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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