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 27433U 02024D 23336.59321035 .00000908 00000-0 50868-3 0 9999
2 27433 99.0360 4.9194 0013762 244.9205 115.0539 14.13234200110231
| Epoch (UTC): | 02 December 2023 14:14:13 |
| Eccentricity: | 0.0013762 |
| inclination: | 99.0360° |
| perigee height: | 838 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 4.9194° |
| argument of perigee: | 244.9205° |
| revolutions per day: | 14.13234200 |
| mean anomaly at epoch: | 115.0539° |
| orbit number at epoch: | 11023 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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