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 02657U 67006A 24338.73044706 -.00000037 00000-0 63701-4 0 9992
2 02657 102.0623 138.8071 0072891 297.3941 74.1816 12.69877408681404
| Epoch (UTC): | 03 December 2024 17:31:50 |
| Eccentricity: | 0.0072891 |
| inclination: | 102.0623° |
| perigee height: | 1326 km |
| apogee height: | 1439 km |
| right ascension of ascending node: | 138.8071° |
| argument of perigee: | 297.3941° |
| revolutions per day: | 12.69877408 |
| mean anomaly at epoch: | 74.1816° |
| orbit number at epoch: | 68140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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