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 11608U 79095B 24282.12709005 .00000238 00000-0 13514-3 0 9998
2 11608 81.2121 139.6870 0053456 220.9761 138.7386 14.06410337305077
| Epoch (UTC): | 08 October 2024 03:03:00 |
| Eccentricity: | 0.0053456 |
| inclination: | 81.2121° |
| perigee height: | 833 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 139.6870° |
| argument of perigee: | 220.9761° |
| revolutions per day: | 14.06410337 |
| mean anomaly at epoch: | 138.7386° |
| orbit number at epoch: | 30507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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