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 60397U 24140U 24358.03420021 .00000267 00000-0 11829-3 0 9999
2 60397 89.0124 335.7320 0042363 145.1798 215.2177 14.19707331 19402
| Epoch (UTC): | 23 December 2024 00:49:14 |
| Eccentricity: | 0.0042363 |
| inclination: | 89.0124° |
| perigee height: | 796 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 335.7320° |
| argument of perigee: | 145.1798° |
| revolutions per day: | 14.19707331 |
| mean anomaly at epoch: | 215.2177° |
| orbit number at epoch: | 1940 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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