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 13497U 78063C 24357.70813997 .00006308 00000-0 12211-2 0 9999
2 13497 74.0534 313.7868 0014243 286.2160 139.6593 14.63459939250763
| Epoch (UTC): | 22 December 2024 16:59:43 |
| Eccentricity: | 0.0014243 |
| inclination: | 74.0534° |
| perigee height: | 672 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 313.7868° |
| argument of perigee: | 286.2160° |
| revolutions per day: | 14.63459939 |
| mean anomaly at epoch: | 139.6593° |
| orbit number at epoch: | 25076 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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